Standards Manager Web Standards List
ESDU-Engineering Sciences Data Unit
Id
1
2
3
4
5
6
7
8
9
10
11
12
Number
75021 E
75020 D
79011 D
19006
20003
20004
19003
88023 C
94035 D
78002 D
78003 D
80025 D
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
18001
18002
18003
18004
18008
18009
18010
18011
19001
19002
19004
19005
00024 A
01015 A
04011 A
08018 A
09001
09002
16004
17004
17008
34
17009
Title
Estimation of the surface pressure fluctuations in the turbulent boundary layer of a flight vehicle
Estimation of far-field sound pressure levels due to buzz-saw noise of a supersonic fan or compressor.
Estimation of noise shielding by barriers
Force limited random vibration testing
Crack resistance curves
Guide to fatigue data available in the Stress and Strength of Components Series
Fatigue strength of shot peened helical tension and compression steel springs
Jet-by-jet shielding of noise
The correction of measured noise spectra for the effects of ground reflection
Evaluation of the attenuation of sound by a uniform atmosphere
Evaluation of the attenuation of broad-band sound by a non-uniform still atmosphere
Mean forces, pressures and flow field velocities for circular cylindrical structures: single cylinder with two-dimensional
flow.
Information on the use of ESDU 18002, ESDU 18003 and ESDU 18004
Form factors for circular sections under combined bending and axial load
Form factors for flanged sections under combined bending and axial load
Form factors for angle, tee and channel sections under combined bending and axial load
An overview of bonded joint design
The estimation of turbulent boundary layer power-law velocity and q profiles from shape factor and momentum thickness
Information on the use of Data Items on powerplant/airframe interactions for propeller-powered aircraft
Cavity oscillations
Fatigue of wrought and cast titanium alloys in bending and under axial loading
Fatigue of wrought and cast Ti-6Al-4V alloys
Guide to the effect of shot peening on fatigue strength
Accumulation of water on runway
The acoustic attenuation of absorbent linings in rectangular flow ducts with application to annular flow ducts
Far-field sound radiation from circular ducts
Prediction of sound attenuation in a refracting turbulent atmosphere with a Fast Field Program
Combination of spectra in Common Data Files from ESDU Aircraft Noise Data Items
Aerodynamics and aero-acoustics of rectangular planform cavities.
Aerodynamics and aero-acoustics of rectangular planform cavities.
Aerodynamics and aero-acoustics of rectangular planform cavities. Part V: Bibliography (up to 2016)
Guide to the use of Data Items in the design of bonded joints
A practical guide to turbulence and flow measurement by thermal anemometry (CTA), laser-Doppler anemometry (LDA)
and particle-image velocimetry (PIV) Part 3: laser-Doppler anemometry
A practical guide to turbulence and flow measurement by thermal anemometry (CTA), laser-Doppler anemometry (LDA)
and particle-image velocimetry (PIV) Part 4: particle-image velocimetry
Year
2020
2020
2020
2020
2019
2019
2019
2019
2019
2019
2019
2019
Organization
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2019
2019
2019
2019
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2019
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2019
2019
2019
2019
2019
2019
2019
2019
2019
2018
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2018
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0
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0
35
36
37
38
39
40
41
17011
13009 A
14014-R2
11005 B
02020 C
00012 C
16001
42
16002
43
44
45
06013 B
76020 B
90034 D
46
47
48
49
50
51
99006 C
AEROW
05.01.01 B
TM165A
TM188
TM189
TM190
52
53
54
55
56
57
58
59
60
61
62
63
TM192
04022
TM183
TM184
TM185
94035 C
90023 E
90005 C
96012 B
77028G
78019 D
82010 D
64
65
66
67
68
69
70
71
82034 B
71006 A
71007 A
72019 C
15001 A
14006
17012
17013
Power spectral density and bandwidth correction of spectrum level
2018
Computer program for calculation of aerodynamic centre of wing-fuselage-nacelle combinations
2018
A theoretically-based method for predicting static-to-flight effects on coaxial jet noise
2018
Prediction of near-field and far-field harmonic noise from subsonic propellers with non-axial inflow
2018
An introduction to aircraft noise
2018
The acoustic attenuation of absorbent linings in cylindrical flow ducts
2018
A practical guide to turbulence and flow measurement by thermal anemometry (CTA), laser-Doppler anemometry (LDA) 2018
and particle-image velocimetry (PIV) Part 1: Overview and Selection of Measurement Technique
A practical guide to turbulence and flow measurement by thermal anemometry (CTA), laser-Doppler anemometry (LDA) 2018
and particle-image velocimetry (PIV) Part 2: constant-temperature anemometry
Propeller slipstream modelling for incidence and sideslip.
2018
Estimation of the maximum discrete frequency noise from isolated rotors and propellers
2018
Computer program for the calculation of normal force and pitching moment of forebody-cylinder combinations at angles of 2018
attack up to 90 degrees and Mach numbers up to 5, including the effects of conical boat-tailing.
Computer-based estimation procedure for near-field single-stream jet noise
2018
KINETIC PRESSURE IN THE WAKE BEHIND A WING
2018
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ESDU TECHNICAL MEMORANDUM Analysis of ground-rolling tests through water with a Canberra aircraft
ESDU TECHNICAL MEMORANDUM Air and ground temperature
ESDU TECHNICAL MEMORANDUM Analysis of tests on a convergent nozzle in an altitude test facility
ESDU TECHNICAL MEMORANDUM Aircraft performance from flight test: An example of the use of manoeuvring
flight
ESDU TECHNICAL MEMORANDUM Analysis of aircraft tests on flooded runways: an empirical approach
An introduction to low-cycle fatigue phenomena
ESDU TECHNICAL MEMORANDUM Compendium of vibration damping data for aerospace structures
ESDU TECHNICAL MEMORANDUM Effects of rear-mounted engine nacelles on sidewash at fin
ESDU TECHNICAL MEMORANDUM Air data calibration using a GPS/INS (EGI)
The correction of measured noise spectra for the effects of ground reflection
Airframe noise prediction
Frequencies of resonance in wind tunnels with ventilated walls and plenum chamber.
Subsonic and transonic base and boat-tail pressure drag of cylindrical bodies with circular-arc boat-tails.
Geometrical characteristics of typical bodies.
Profile drag of axisymmetric bodies at zero incidence for subcritical Mach numbers
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to sideslip, (Y sub v) sub F, (N sub v)
sub F, (L sub v) sub F, in the presence of body, wing and tailplane.
Aircraft forces due to interference between a jet efflux and a slotted flap.
Low-speed longitudinal aerodynamic characteristics of slender wings.
Low-speed normal force and pitching moment of slender wings in ground effect.
Buckling of flat isotropic plates under uniaxial and biaxial loading.
Aircraft performance from flight test Part 1: derivation of a mathematical model
Prediction of loads in shear cleat attachments
Combination of levels in dB
Aircraft performance from flight test. Part 3: in-flight calibration of an angle of attack sensor
2018
2018
2018
2018
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2018
2018
2017
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2017
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2017
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72
73
74
75
76
77
78
79
16005
16006
16008
17002
17003
64001 K
16008
15009
80
81
82
83
84
85
15010
13003
15003 A
14014
00010
98019 D
86
87
88
89
90
91
92
93
94
95
96
05001 A
99035
13003-R1
16003
75028 A
75031 D
74036 C
15011
89047 D
90029 C
AEROC
04.01.04 D
AEROC
08.01.01 B
97
98
99
100
101
102
103
104
105
106
107
AEROF
01.01.08 D
99003 A
AEROA
06.01.00 K
AEROA
07.01.00 I
93016 C
85029 B
85046 E
98008 C
TM 161 B
15004
Mass flow rate of a leak into an external stream
2017
Drag due to a leak discharging into an external stream
2017
Frictional and retarding forces on aircraft tyres Introduction to the ESDU methods
2017
Octave and fractional-octave band filters
2017
Fatigue crack propagation rates and threshold stress intensity factors in high strength low alloy steel plate, bar and forgings. 2017
Guide to stress concentration data
2017
Frictional and retarding forces on aircraft tyres Introduction to the ESDU methods
2017
Determination of hydroplaning speeds and corresponding hydrodynamic forces for rib tread aircraft tyres Application of
2016
ESDU 15003
Coupling loss factors
2016
Modal density of acoustic spaces
2016
Planing of rib-tread aircraft tyres
2016
A theoretically-based method for predicting static-to-flight effects on coaxial jet noise
2016
Aircraft Noise Series: Record of Documents - Issue 23
2016
Computer-based estimation procedure for single-stream jet noise Including far-field, static jet mixing noise database for
2016
circular nozzles
Prediction of combustor noise from gas turbine engines
2016
Performance Series record of documents - Issue 28
2016
Modal density of acoustic spaces
2016
Aircraft performance from flight test Part 2: thrust-drag accounting
2016
Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds.
2016
Drag of two-dimensional steps and ridges immersed in a turbulent boundary layer for Mach numbers up to 3
2016
Drag due to a circular cavity in a plate with a turbulent boundary layer at subsonic, transonic and supersonic speeds.
2016
Acoustics of reverberation chambers
2016
In-plane forces and moments on installed inclined propellers at low forward speeds.
2016
An introduction to aircraft excrescence drag
2016
EFFECT OF IRVING INTERNAL BALANCE ON HINGE-MOMENT COEFFICIENT IN TWO-DIMENSIONAL
2016
FLOW
RATE OF CHANGE OF PITCHING MOMENT COEFFICIENT WITH CONTROL
2016
DEFLECTION FOR A PLAIN CONTROL IN INCOMPRESSIBLE
TWO-DIMENSIONAL FLOW, m0
LIFT COEFFICIENT INCREMENT DUE TO FULL-SPAN SLOTTED FLAPS
2015
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Generation of GUNACA 23-series of low-drag aerofoils.
Information on the use of Data Items on rolling moment derivatives of an aircraft
2015
2015
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Information on the use of Data Items on yawing moment and sideforce
derivatives of an aircraft
Parameter estimation of linear systems from frequency response measurements (Computer program)
Calculation of ground performance in take-off and landing.
Quadrature methods for the evaluation of definite integrals
Prediction of noise generated by fans and compressors in turbojet and turbofan engines
Calculation of coefficients of rolling, braking and yawed rolling resistance
Stress concentration factors in keyways
2015
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0
2015
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0
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108
109
110
111
112
113
114
115
116
117
118
119
120
TM 174A
15005
00001
82037 F
13007 B
14007
TM 176A
AERO
C.08.01.01 B
15007
AERO
A.07.01.00 I
10002 B
121
122
123
15006
AERO
A.06.01.00 K
TM 180
10003 B
86021 D
124
125
126
127
128
129
130
15008
05011 D
10004 B
13005 A
15012
10015 B
13002 A
131
132
133
134
135
136
137
138
72023 A
11004 C
89029 B
15001
15002
88031 E
91017 F
11002 A
139
140
141
142
143
91004 A
13006
90010 C
14005
88040 C
Correlation of the micro-texture sharpness parameter F1
Stress concentration factors for optimised holes in flat plate
Aerodynamics Series: Record of Documents - Issue 26
The response of two-degree-of-freedom systems (computer program)
Side-force coefficients on aircraft tyres in yawed and unbraked motion on dry and wet pavements
Selection of roughness bands to induce boundary-layer transition in wind-tunnel testing
Effective phase angle in tyre-friction modelling
RATE OF CHANGE OF PITCHING MOMENT COEFFICIENT WITH CONTROL DEFLECTION FOR A PLAIN
CONTROL IN INCOMPRESSIBLE TWO-DIMENSIONAL FLOW, m sub zero
Worked example for tyre in yawed motion on a dry or wet runway surface An application of ESDU 13007
Information on the use of Data Items on yawing moment and sideforce derivatives of an aircraft
2015
2015
2015
2015
2015
2015
2015
2015
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0
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2015
2015
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Introduction to worked examples of tyres rolling or braking on dry or precipitate contaminated runways. Application of
ESDU 05011 and ESDU 13007
Stress concentration factors for optimised notches and fillets in flat plate
Information on the use of Data Items on rolling moment derivatives of an aircraft
2015
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0
2015
2015
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Modelling of ventilation for thermal comfort and indoor air quality
Worked example for tyre in linear motion on a contaminated runway surface. An application of ESDU 05011
Introduction to aerodynamic derivatives, equations of motion and stability (including the classical criteria of longitudinal
stability and control, and description of the lateral modes of motion)
Tyre in linear motion on a runway covered by various forms of loose snow. An application of ESDU 05011
Summary of the model for performance of an aircraft tyre rolling or braking on dry or precipitate contaminated runways
Worked example of ground-test machine operating on a dry or contaminated runway surface. Application of ESDU 05011
Information on the use of Data Items on the longitudinal stability of aircraft
Flow in rotating cavities
Model for performance of a single aircraft tyre rolling or braking on dry and precipitate contaminated runways
Worked example for aircraft with multiple-wheel undercarriages braking on water-covered runway. Application of ESDU
11004
Low-speed longitudinal aerodynamic characteristics of aircraft in ground effect
Decelerating forces on multiple-wheel undercarriages rolling or braking on precipitate contaminated runways
Installed tailplane lift-curve slope at subsonic speeds
Aircraft performance from flight test Part 1: derivation of a mathematical model
Definitions for runway contaminants and the classification and distribution of hard runway surfaces
Lift and longitudinal forces on propeller/nacelle/wing/flap systems
Statistical methods applicable to analysis of aircraft performance data
The prediction of the far-field mixing noise from coaxial subsonic jets based on a database for stationary coplanar conical
nozzles
Pitching moment derivative due to rate of pitch for projectiles at supersonic speeds
ESDUperf: aircraft performance program
Pitching moment and lift force derivatives due to rate of pitch for aircraft at subsonic speeds
Lift and rolling moment due to spoilers on wings at subsonic speeds with trailing-edge flaps deployed
Program for calculation of aileron rolling moment and yawing moment coefficients at subsonic speeds
2015
2015
2015
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0
2015
2015
2015
2015
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2015
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2015
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2015
2014
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0
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0
0
2014
2014
2014
2014
2014
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0
0
0
0
0
144
145
14004
87008 I
146
13014
147
148
149
AERO
F.01.01.08 D
00025 A
13012
150
151
TM 172
85010 A
152
153
154
TM 178
02011
13013
155
156
157
158
159
160
161
162
10011 A
96026 C
13007 A
91009 B
83044
83044-R1
84027 D
98005 D
163
AEROF
02.01.08 E
09009 B
81014 A
164
165
166
167
168
169
170
171
172
173
174
175
176
177
00032 E
14003
AERO
F.02.01.08 E
73017 C
13001
66011 A
71027 A
76016 B
00033 D
12006
02016-R1
73002 B
Lift and rolling moment due to spoilers on wings at subsonic speeds with trailing-edge flaps undeployed
Rudder sideforce, yawing moment and rolling moment control derivatives at low speeds: Y sub zeta, N sub zeta and L sub
zeta
Viscous full-potential (VFP) method for three-dimensional wings and wing-body combinations Part 3: Error messages,
failures and suggested remedies
LIFT COEFFICIENT INCREMENT DUE TO FULL-SPAN SLOTTED FLAPS
2014
2014
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2014
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2014
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Computer program for prediction of aircraft lateral stability derivatives in sideslip at subsonic speeds
Viscous full-potential (VFP) method for three-dimensional wings and wing-body combinations Part 2: Use of VFP and
related programs
Derivation of part span factors for lift and rolling moment
Estimation of sideforce, yawing momentand rolling moment derivatives dueto rate of roll for complete aircraftat subsonic
speeds
Effect of wing-mounted engine nacelles of propeller-driven aircraft on lateral stability derivatives in sideslip
Wind Engineering Series organisation: preface sections and data items location schedule amendment record - Issue 8
Viscous full-potential (VFP) method for three-dimensional wings and wing-body combinations. Part 1: Validation of VFP
results with experiment and comparisons with other methods.
Endurance of titanium and titanium alloy structural elements subjected to simulated acoustic loading
Drag and yawing moment due to spoilers
Side-force coefficients on aircraft tyres in yawed and unbraked motion on dry and wet pavements
Effect of twin fins on isolated tailplane lift-curve slope
Plasticity correction factors for plate buckling
Plasticity correction factors for plate buckling
Endurance of fibre-reinforced composite, laminated structural elements subjected to simulated random acoustic loading.
Design and performance evaluation of heat exchangers: the effectiveness-NTU method. Part 3: graphical and analytical
data. - Incorporates A, B, and C
VORTEX DRAG COEFFICIENT OF WING WITH PART-SPAN FLAP AND CENTRAL CUT-OUT
2014
2014
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2014
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2014
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2014
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2014
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2013
ESDU
0
Aircraft noise prediction
Contribution of wing planform to derivatives of yawing moment and sideforce due to roll rate at subsonic speeds, (Np)w
and (Yp)w
Aircraft Performance Program Part 2: Installing and running Programs APP02 and APP03
Guide to bolted joints and screw threads data
VORTEX DRAG COEFFICIENT OF WING WITH PART-SPAN FLAP AND CENTRAL CUT-OUT
2013
2013
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0
2013
2013
2013
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Reynolds number, speed of sound, dynamic viscosity, kinetic pressure and total pressure coefficient in air
The prediction of shock noise from supersonic jets including the near-field
Loaded pins in axially loaded bars. Maximum elastic stress at hole boundary
Endurance of high strength steels (in bending)
Generalisation of smooth continuous stress-strain curves for metallic materials
Aircraft Performance Program Part 3: Brief guide Programs APP02, APP03
Method to determine surface finish required to minimise local skin friction in the presence of a turbulent boundary layer.
Fracture toughness (KIc) values of some cast irons
Fatigue of steel spline assemblies under reversed torsion
2013
2013
2013
2013
2013
2013
2013
2013
2013
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178
179
180
181
182
183
81012
83040 D
82012-R1
82022-R1
81029-R1
82009 E
184
185
186
187
188
189
190
80004-R1
81007-R1
81011-R1
81012-R1
76016 B-R1
78016-R1
78023 A-R1
191
192
79010-R1
78036 A-R1
193
194
195
196
197
198
199
78043 A-R1
78013 B
76032-R1
77011-R1
75016-R1
76007-R1
76014 B-R1
200
201
202
203
73002 B-R1
71027 A-R1
73004 A-R1
74016-R1
204
205
206
207
208
209
210
211
212
213
214
215
71009 A-R1
70016 B-R1
67019 A-R1
66011 A-R1
67014 A-R1
00035 E
81011
83040 D
00011
TM 173
73004 A
81029
Fatigue threshold stress intensity factors and slow crack propagation rates in low and medium strength low alloy steel
2013
Method for the rapid estimation of spanwise loading of wings with camber and twist in subsonic attached flow
2013
Nested helical compression springs of round wire (To be used in conjunction with ESDU 82008)
2013
Endurance of steel lugs with clearance-fit pins (Tensile mean stress)
2013
Stress intensity factors in lugs (through-thickness cracks)
2013
Compressible flow of gases. Pressure losses and discharge coefficients of orifice plates, perforated plates and thick orifice 2013
plates in ducts.
Fatigue strength of steel coned disc springs (Tentative)
2013
Fatigue strength in bending of steel I-beams with welded attachments
2013
Fatigue crack propagation in low and medium strength low alloy steel plate, bar and forgings
2013
Fatigue threshold stress intensity factors and slow crack propagation rates in low and medium strength low alloy steel
2013
Generalisation of smooth continuous stress-strain curves for metallic materials
2013
The effect of post-weld treatments on fatigue at fillet welded attachments
2013
Fatigue strength of transverse fillet welded joints and attachments in steels
2013
under bending loading
Characteristics of disc springs in combination (to be used in conjunction with ESDU 78043)
2013
The compounding method of estimating stress intensity factors for cracks in complex configurations using solutions from 2013
simple configurations
Single disc springs - elastic deflections, stresses, stiffnesses and resiliences
2013
Aerodynamic centre of wing-fuselage-nacelle combinations: effect of rear-fuselage pylon-mounted nacelles
2013
Fatigue strength of longitudinal flange-to-web welds in steel I-beams and T-sections
2013
Fatigue strength of transverse butt welds in steel plate under axial loading
2013
Fatigue strength of transverse fillet and cruciform butt welds in steels
2013
Fatigue strength of longitudinal fillet welded attachments and joints in steels under axial loading
2013
Estimation of endurance and construction of constant amplitude S N curves from related data corrected for notch and mean 2013
stress effects
Fatigue of steel spline assemblies under reversed torsion
2013
Endurance of high strength steels (in bending)
2013
Criteria of yielding for ductile materials under static loading
2013
The fatigue strength at high endurance of notched low alloy steel specimens (in bending and under axial loading, zero mean 2013
stress)
Design against fatigue Design principles
2013
Terms and notation for fatigue endurance data.
2013
Static strength of screwed fasteners
2013
Loaded pins in axially loaded bars. Maximum elastic stress at hole boundary
2013
Fatigue strength of thick cylinders under internal pressure
2013
Aircraft Performance Program Part 5: Detailed input and output Program APP02
2013
Fatigue crack propagation in low and medium strength low alloy steel plate, bar and forgings
2013
Method for the rapid estimation of spanwise loading of wings with camber and twist in subsonic attached flow
2013
Vibration and Acoustic Fatigue Series: Record of Documents - Issue 9
2013
Material damping of metals and alloys
2013
Criteria of yielding for ductile materials under static loading
2013
Stress intensity factors in lugs (through-thickness cracks)
2013
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0
0
216
217
218
219
220
221
222
223
224
85011 B
09014 A
82011 C
TM 95
81007
00034 E
13007
82012
74016
225
226
227
228
229
230
231
232
233
234
00036 D
82022
75016
13009
06011 A
76007
67014 A
76015 D
87031 C
DWN 10009
235
236
237
238
239
240
241
242
243
76032
77012 B
13004
00038 D
09016
03003
02016
71009 A
76014 B
244
245
246
247
248
249
250
251
252
253
94036 A
02020 B
77011
00031 E
00039 C
67019 A
12003
84030 C
75021 D
82007
Pitot and static errors due to non-steady flight
2013
Elastic stress concentration factors. Geometric discontinuties in flat bars or strips of isotropic material
2013
Estimation of sideforce and yawing moment derivatives due to sideslip for complete aircraft at subsonic speeds
2013
Impact forces resulting from wheel generated spray: a re-assessment of existing data
2013
Fatigue strength in bending of steel I-beams with welded attachments
2013
Aircraft Performance Program Part 4: Brief form of input and output Programs APP02, APP03
2013
Side-force coefficients on aircraft tyres in yawed and unbraked motion on dry and wet pavements
2013
Nested helical compression springs of round wire (To be used in conjunction with ESDU 82008)
2013
The fatigue strength at high endurance of notched low alloy steel specimens (in bending and under axial loading, zero mean 2013
stress)
Aircraft Performance Program Part 6: Examples of application Programs APP02 and APP03
2013
Endurance of steel lugs with clearance-fit pins (Tensile mean stress)
2013
Fatigue strength of transverse fillet and cruciform butt welds in steels
2013
Computer program for calculation of aerodynamic centre of wing-fuselage-nacelle combinations
2013
Spectral methods for the estimation of fatigue life
2013
Fatigue strength of longitudinal fillet welded attachments and joints in steels under axial loading
2013
Fatigue strength of thick cylinders under internal pressure
2013
Aerodynamic centre of wing-fuselage combinations
2013
Wing angle of attack for zero lift at subcritical Mach numbers
2013
Computer program for estimation of the performance of aircraft type tyres rolling or braking on dry and precipitate
2013
contaminated runways - Issue 7
Fatigue strength of longitudinal flange-to-web welds in steel I-beams and T-sections
2013
Aerodynamic centre of wing-fuselage-nacelle combinations: effect of wing-pylon mounted nacelles
2013
Selection of cooling systems
2013
Aircraft Performance Program Part 8: description of APP02
2013
Use of local-flow conditions for calculation of roughness-particle height in transition strips on wings
2013
Stress and Strength Series organisation: preface amendment record - Issue 3
2013
Fracture toughness (KIc) values of some cast irons
2013
Design against fatigue Design principles
2013
Estimation of endurance and construction of constant amplitude S N curves from related data corrected for notch and mean 2013
stress effects
The prediction of sound attenuation as a result of propagation close to the ground
2013
An introduction to aircraft noise
2013
Fatigue strength of transverse butt welds in steel plate under axial loading
2013
Aircraft Performance Program Part 1: Introduction to the computer programs for aircraft performance evaluation
2013
Aircraft Performance Program Part 9: Testing programs APP02 and APP03
2013
Static strength of screwed fasteners
2013
Pressure and Flow Measurements
2012
Longitudinal turbulence intensities over terrain with roughness changes
2012
Estimation of the surface pressure fluctuations in the turbulent boundary layer of a flight vehicle
2012
Structural Members: mean fluid forces on members of various cross sections
2012
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
ESDU
ESDU
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ESDU
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ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
254
01014 A
255
256
14001
93030 A
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
82031 B
95026
DWN 10020
84015 A
93013
77014 B
85012 C
84011 D
DWN 10018
91010 A
76003 C
84003 B
70012 E
96027 A
91001
83036 B
12001
74029 E
89042 A
70011 J
89050 B
85021 C
TM 168
TM 175
88023 B
83035 F
10023 A
89036 B
83045 C
81018 B
TM 169
288
289
290
291
292
06010 A
88038
64001
74029 E-R1
75021 D-R1
Frictional pressure gradient in adiabatic flows of gas-liquid mixtures in horizontal pipes: prediction using empirical
correlations and database
Applying, measuring and maintaining pretension in steel bolts
Three-dimensional elastic stress concentration factors Plain or countersunk hole in a wide plate subjected to tension,
bending or pin loading
Paraboloidal antennas: wind loading. Part 1: mean forces and moments
Edge effects on the response of sandwich panels subjected to acoustic loading
Dynamic characteristics of cylindrical helical springs. Part 4: examples and computer program - Issue 8
Cylinder groups: mean forces on pairs of long circular cylinders
Lift-curve slope for structural response calculations
Flat panels in shear Post-buckling analysis
Estimation of damping in laminated and fibre-reinforced plates
Wind speed profiles over terrain with roughness changes
Aerodynamics Fixes on Aircraft - Issue 6
Response of structures to galloping excitation Background and approximate estimation
Geometrical properties of cranked and straight-tapered wing planforms
Fatigue crack propagation rates and threshold stress intensity factors in high alloy and corrosion resistant (stainless) steel
Lift-curve slope and aerodynamic centre position of wings in inviscid supersonic flow
Estimation of the unsteady lift coefficient of subsonic propeller blades in non-axial inflow
Structural parameters used in response calculations Estimation of numerical values
Natural frequencies of rectangular, specially orthotropic laminated plates
Prediction of turbine noise from aero-engines
Friction losses for fully-developed flow in straight pipes of constant cross section subsonic compressible flow of gases
Body effect on wing angle of attack and pitching moment at zero lift at low speeds
Lift-curve slope and aerodynamic centre position of wings in inviscid subsonic flow
Boundary walls, fences and hoardings: mean and peak wind loads and overturning moments
Analysis of pretensioned bolted joints subject to tensile (separating) forces
Derivation of equations for the geometrical properties of straight-tapered and multi-panel wings
Self-loosening of bolted joints
Jet-by-jet shielding of noise
Estimation of the stiffnesses and apparent elastic properties of laminated flat plates
Computer program for calculation of equivalent straight-tapered wing planform
The calculation of overground sound propagation in the presence of wind and temperature gradients
Strong winds in the atmospheric boundary layer Part 2: discrete gust speeds
Natural frequencies of thick-walled isotropic circular-cylindrical shells (shear diaphragm end conditions)
Wing lift-curve slope in inviscid subsonic flow: Improvements to the Helmbold-Diederich equation and comparison with
data from ESDU 70011
Cycle counting methods for the estimation of fatigue life
Estimation of hours per year when mean wind speed exceeds specified thresholds
Guide to stress concentration data.
Friction losses for fully-developed flow in straight pipes of constant cross section subsonic compressible flow of gases
Estimation of the surface pressure fluctuations in the turbulent boundary layer of a flight vehicle
2012
ESDU
0
2012
2012
ESDU
ESDU
0
0
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
2012
2012
2012
2012
2012
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
293
294
81018 B-R2
80040G-R2
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
80020 B
82031 B-R1
82007-R1
83009 C-R1
83020-R1
04021
83020
88037
97021 A
04022-R1
06009 A
11009
87035 B
TN 07007 B
90029 B
TM 170
14002
04022
88033 A
314
315
316
317
87034 B
04006 B
83009 C
TM169
318
319
320
321
322
323
324
325
326
327
328
329
330
331
84011 D-R1
84015 A-R1
83045 C-R1
84030 C-R1
83036 B-R2
85012 C-R2
85021 C-R1
87034 B-R1
87035 B-R1
88037-R1
88038-R1
93013-R1
96027 A-R3
95026-R2
Natural frequencies of thick-walled isotropic circular-cylindrical shells (shear diaphragm end conditions).
Free vibration of thin-walled, orthogonally stiffened, circularcylindrical
shells
Average downwash at the tailplane at low angles of attack and subsonic speeds
Paraboloidal antennas: wind loading. Part 1: mean forces and moments
Structural Members: mean fluid forces on members of various cross sections
Damping of structures Part 1: tall buildings
Paraboloidal antennas: wind loading. Part 2: surface pressure distribution
Fluid Mechanics, Internal Flow Series: Record of Documents - Issue 15
Paraboloidal antennas: wind loading. Part 2: surface pressure distribution
World-wide extreme wind speeds. Part 2: examples using various methods of analysis
Effect of trailing-edge flap deployment on average downwash at the tailplane at low speeds
An introduction to low-cycle fatigue phenomena
Fatigue damage and life under random loading.
Compendium of modal densities Part II: Shell structures
Calculation methods for along-wind loading Part 2: response of line-like structures to atmospheric turbulence
Incompressible flow through orifice plates a review of the data in the literature
An introduction to aircraft excrescence drag
Falcon 20: rolling on dry and snow-covered surfaces
Lock nuts and other thread locking devices
An introduction to low-cycle fatigue phenomena
The design of spur and helical involute gears. A procedure compatible with BS 436: Part 3: 1986 method for calculation of
contact and root bending stress limitations for metallic involute gears
World-wide extreme wind speeds Part 1: origins and methods analysis
Pressure gradient in upward adiabatic flows of gas-liquid mixtures in vertical pipes
Damping of structures Part 1: tall buildings
ESDU TECHNICAL MEMORANDUM Wing lift-curve slope in inviscid subsonic flow: Improvements to the HelmboldDiederich equation and comparison with data from ESDU 70011
Wind speed profiles over terrain with roughness changes
Cylinder groups: mean forces on pairs of long circular cylinders
Strong winds in the atmospheric boundary layer Part 2: discrete gust speeds
Longitudinal turbulence intensities over terrain with roughness changes
Natural frequencies of rectangular, specially orthotropic laminated plates
Estimation of damping in laminated and fibre-reinforced plates
Analysis of pretensioned bolted joints subject to tensile (separating) forces
World-wide extreme wind speeds Part 1: origins and methods analysis
Calculation methods for along-wind loading Part 2: response of line-like structures to atmospheric turbulence
World-wide extreme wind speeds. Part 2: examples using various methods of analysis
Estimation of hours per year when mean wind speed exceeds specified thresholds
Lift-curve slope for structural response calculations
Estimation of the unsteady lift coefficient of subsonic propeller blades in non-axial inflow.
Edge effects on the response of sandwich panels subjected to acoustic loading.
2012
2012
ESDU
ESDU
0
0
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
2012
2012
2012
2012
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
2012
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
332
93030 A-R1
333
334
335
336
337
338
339
340
341
91001-R1
91010 A-R1
89050 B-R1
88023 B-R1
89036 B-R1
90016 B-R1
91013 A-R1
91025 E-R1
93031 A-R1
342
343
344
345
346
347
92042 B-R1
93022 B-R1
89011 A-R1
89030 A-R1
88022 C-R1
86024 E-R1
348
349
350
351
352
353
87002 C-R1
85037 D-R1
84008 D-R1
72005 E
82019
00007 B
354
11007
355
356
357
358
359
07001
91025 E
73014 A
97030 A
92014 D
360
361
362
11008
07002 A
93031 A
363
364
365
366
367
07001 ADD
00002-R1
10023 B
00024
10016
Three-dimensional elastic stress concentration factors Plain or countersunk hole in a wide plate subjected to tension,
2012
bending or pin loading
Structural parameters used in response calculations Estimation of numerical values
2012
Response of structures to galloping excitation Background and approximate estimation
2012
Boundary walls, fences and hoardings: mean and peak wind loads and overturning moments
2012
Jet-by-jet shielding of noise
2012
The calculation of overground sound propagation in the presence of wind and temperature gradients
2012
Natural frequencies of isotropic and orthotropic rectangular plates under static in-plane loading (including shear loading)
2011
Methods for improving damping Part 2: layered damping treatment for structures: analysis and examples
2011
Non-Newtonian fluids: Frictional pressure loss prediction for fully-developed flow in straight pipes
2011
Pipeline vibrations. Computer program for the prediction of fluid transients in flexible, unbranched three-dimensional
2011
piping systems
Ejectors and jet pumps: Computer program for design and performance for compressible gas flow
2011
Ejectors and jet pumps: computer program for design and performance for liquid flow
2011
Natural frequencies of singly-curved laminated plates with simply-supported edges
2011
Pipeline Vibrations Fluid transients in non-rigid, unbranched planar piping systems
2011
Pipeline Vibrations Undamped natural vibration of pipelines
2011
Estimation of rms strain in laminated face plates of simply-supported sandwich panels subjected to random acoustic
2011
loading. Including a simplified natural frequency prediction method
Natural frequencies of rectangular singly-curved plates
2011
Natural frequencies of simply-supported sandwich panels with laminated face plates
2011
Estimation of r.m.s. strain in laminated skin panels subjected to random acoustic loading
2011
The estimation of r.m.s. stress in stiffened skin panels subjected to random acoustic loading
2011
Undamped natural vibration of rectangular sway frame buildings and frame structures
2011
Drag of a rectangular planform cavity in a flat plate with a turbulent boundary layer for Mach numbers up to 3. Part II:
2011
Open and transitional flows
Full-potential method for three-dimensional wings and wing-body combinations Part 6: Full-potential with frozen boundary 2011
layer
Noise transmission into aircraft cabins
2011
Non-Newtonian fluids: Frictional pressure loss prediction for fully-developed flow in straight pipes
2011
The estimation of r.m.s. stress in skin panels with flexible stiffeners subjected to random acoustic loading
2011
VGK method for two-dimensional aerofoil sections Part 3: estimation of a separation boundary in transonic flow
2011
Blending profiles of disc cams with radial translating roller followers. Part 1: to reduce segment angle, reduce reference
2011
circle radius or increase follower lift
Compendium of modal densities Part 1: rods, beams and plates
2011
Wing viscous drag coefficient in shock-free attached flow
2011
Pipeline vibrations. Computer program for the prediction of fluid transients in flexible, unbranched three-dimensional
2011
piping systems
Noise transmission into aircraft cabins Addendum Estimation of section properties of fuselage stiffeners
2011
Sound power radiation from isotropic plates
2011
Computer program for calculation of equivalent straight-tapered wing planform
2011
The acoustic attenuation of absorbent linings in rectangular flow ducts with application to annular flow ducts
2011
Drag of a rectangular planform cavity in a flat plate with a turbulent boundary layer for Mach numbers up to 3. Part III :
2011
Effect of doors
ESDU
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
ESDU
0
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
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0
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0
0
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
TM 165
Analysis of ground-rolling tests through water with a Canberra aircraft
TN 10013
CFD validation studies for incompressible flow through square-edged orifice plates
96002
Geneva mechanisms. Part 1: design
74033 A-R1
Estimation of sound pressure levels due to buzz-saw noise within the intake duct of a supersonic fan or compressor
74025 B-R1
Natural frequencies of box structures
73014 A-R1
The estimation of r.m.s. stress in skin panels with flexible stiffeners subjected to random acoustic loading
72005 E-R1
The estimation of r.m.s. stress in stiffened skin panels subjected to random acoustic loading
91013 A
Methods for improving damping Part 2: layered damping treatment for structures: analysis and examples
10019
Effect of link length tolerances on the performance of four-bar linkages
91008 A
Strength of lugs under axial load
92042 B
Ejectors and jet pumps: Computer program for design and performance for compressible gas flow
10022
Trailing-vortex drag coefficient in shock-free attached flow cambered and twisted wings
DWN TN10013 CFD validation studies for incompressible flow through square-edged orifice plates - Issue 5
CFD-BPG
CFD Best Practice Guidelines for modelling pressure losses and flow characteristics in square-and knife-edged orifice
11010
plates
97031
Estimation of shelter provided by solid and porous fence
10017
A guide to the alleviation of the base drag of a flat plate with a blunt trailing edge
11005
Prediction of near-field and far-field harmonic noise from subsonic propellers with non-axial inflow
74025 B
Natural frequencies of box structures
82027 B
Estimation of lateral attenuation of air-to-ground jet or turbofan aircraft noise in one-third octave bands
07003 A
Modelling of wing viscous drag coefficient in shock-free attached flow
08018
Combination of spectra in Common Data Files from ESDU Aircraft Noise Data Items
TM 167
Mumeter Mk 6: a continuous friction measuring device. Evaluation on test surfaces at Nantes
95001 A
Kinematic analysis of disc cams
00024
The acoustic attenuation of absorbent linings in rectangular flow ducts with application to annular flow ducts
93002 B
Blending profiles of disc cams with radial translating roller followers. Part 2: to incorporate an intermediate precision point
or a constant velocity component
TM 101
Derivation of lubricant entrainment velocity for disc cams with six different types of follower
92005 D
Minimum size of disc cams with radial translating roller followers
76020 A
Estimation of the maximum discrete frequency noise from isolated rotors and propellers
78002 C
Evaluation of the attenuation of sound by a uniform atmosphere
85037 D
Natural frequencies of simply-supported sandwich panels with laminated face plates
74033 A
Estimation of sound pressure levels due to buzz-saw noise within the intake duct of a supersonic fan or compressor
84008 D
Estimation of r.m.s. strain in laminated skin panels subjected to random acoustic loading
99006 B
Computer-based estimation procedure for near-field single-stream jet noise
00002
Sound power radiation from isotropic plates
01015
Far-field sound radiation from circular ducts
89011 A
Natural frequencies of singly-curved laminated plates with simply-supported edges
06002A
Dwell-Rise-Fall-Dwell and Dwell-Fall-Rise-Dwell cam laws Sections 1 to 8: segments having equal rise and fall periods
86024 E
Estimation of rms strain in laminated face plates of simply-supported sandwich panels subjected to random acoustic
loading. Including a simplified natural frequency prediction method
13016
Some factors affecting the design of bolted assemblies
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
2011
ESDU
0
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
TM 96
04011
09006
00004
87002 C
78003 C
93022 B
91043 C
TM 102
00006 B
Operations on surfaces covered with slush
Prediction of sound attenuation in a refracting turbulent atmosphere with a Fast Field Program
Material Damping
Mechanisms Series record of documents - Issue 11
Natural frequencies of rectangular singly-curved plates
Evaluation of the attenuation of broad-band sound by a non-uniform still atmosphere
Ejectors and jet pumps: computer program for design and performance for liquid flow
Mean wind speeds over hills and other topography
Derivation of contact force and radius of curvature of cam profile for disc cams with six different types of follower
Drag of a rectangular planform cavity in a flat plate with a turbulent boundary layer for Mach numbers up to 3. Part I:
Closed flow
TN 08009 A
CFD validation studies for transitional flow in circular straight pipes with smooth walls
02009
Sound radiation from orthotropic rectangular plates Part I: Estimation by asymptotic method
86035 E
Integral length scales of turbulence over flat terrain with roughness changes
81036 A
Undamped natural vibration of core buildings
89030 A
Pipeline Vibrations Fluid transients in non-rigid, unbranched planar piping systems
88022 C
Pipeline Vibrations Undamped natural vibration of pipelines
86026 C
Introduction to polynomial cam laws
94035 B
The correction of measured noise spectra for the effects of ground reflection
90016 B
Natural frequencies of isotropic and orthotropic rectangular plates under static in-plane loading (including shear loading)
11006
Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (ii) Comparison of extrapolated lowReynolds-number lift measurements on the F4 wing/body with high-Reynolds-number measurements
94011 C
Contact stress in disc cams with domed or flat faced followers
05009
Heat Transfer Series record of documents - Issue 2
03012 B
Computer program for calculation of mean value properties for non-uniform compressible flows
SPC-M13-1
Oct.09: Mathematical modeling of asphaltenes deposition and removal in crude distillation units
10012
Application of linear regression analysis to acoustic fatigue data
09015
EXTRAPOLATING WIND-TUNNEL DATA TO FULL-SCALE REYNOLDS NUMBER Part 3: Example (i) Choice of
simulation criteria and transition-strip locations for the F4 Wing/Body combination at the design condition
SPG-M12-1
Sept.09: Fouling in refinery preheat trains. PHT network simulation
PERF ED 1/1 A Approximate estimation of drag of windmilling propellers
SPA-M12-2
Sept.09: Application of ATR-FTIR imaging to study precipitation due to heating of crude oil
SPA-M6-1
Apr.08: Characterization of asphaltenes and deposited foulants
PERF ED 1/2 A Approximate estimation of braking thrust of propellers (piston engines)
SPA-M14-1
Sept.10: Characterization of Asphaltenes and Deposited Foulants
SPG-M15-2
Refinery preheat train modelling, simulation and performance improvement
93005 A
Calculation methods for steadily loaded axial groove hydrodynamic journal bearings (Guide to use of computer program
A9305)
SPD-M13-2
Oct.09: Simulation of asphaltene-hydrocarbon containing systems
SPC-M15-1
Sept.10: Mathematical modeling of asphaltenes deposition and removal in crude distillation units
SPG-M12-2
Sept.09: Modelling of fouling in heat exchangers: Overview, recent results and opportunities
SPF-M12-1
Sept.09: Annulus flow tests (status report on tube and annulus flow rig development)
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
2011
2011
2011
2011
2011
2011
2011
2011
2011
2011
ESDU
ESDU
ESDU
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ESDU
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0
0
0
0
0
0
0
0
0
0
2010
2010
2010
2010
2010
2010
ESDU
ESDU
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0
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0
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0
2010
2010
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2010
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2010
2010
ESDU
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ESDU
ESDU
ESDU
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ESDU
0
0
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0
0
0
0
0
2010
2010
2010
2010
ESDU
ESDU
ESDU
ESDU
0
0
0
0
445
446
447
448
449
450
451
452
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461
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476
477
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479
480
481
482
00015 A
SPC-M11-1
SPA-M12-1
10014
Disc cams: tribological analysis using computer program A0015
Apr.09: Modeling of asphaltenes deposition and removal in crude-oil distillation units
Sept.09: Characterisation of petroleum fouling with respect to operational parameters: an experimental study
Full-potential method for three-dimensional wings and wing-body combinations Part 5: Pre-processor to represent effect of
fore- and aft-body shape on wing flow
SPG-M10-2
Apr.09: Advanced modelling and simulation of PHT hot-end exchangers for fouling mitigation
04024 B
An introduction to rigid aeroplane response to gusts and atmospheric turbulence
SPD-M13-1
Oct.09: Modelling asphaltenes using SAFT or related approaches
93004 A
Calculation methods for steadily loaded central circumferential groove hydrodynamic journal bearings. (Guide to use of
computer program A9304)
94008 C
Lubricant film thickness between disc cams and followers
04017
Fatigue Endurance Data Series organisation: preface amendment record - Issue 2
10011
Endurance of titanium and titanium alloy structural elements subjected to simulated acoustic loading
96011 C
Geneva mechanisms. Part 2: computer program
00012 B
The acoustic attenuation of absorbent linings in cylindrical flow ducts
SPC-M7-1
Apr.08: Modelling of asphaltenes deposition and removal in crude distillation units
SPG-M10-1
Apr.09: Simulating refinery preheat trains subject to fouling - operational control strategies
93001 D
Contact stress in disc cams with roller followers
92037 A
Calculation methods for externally pressurised (hydrostatic) journal bearings with capillary restrictor control (Guide to use
of computer program A9237)
SPD-M10-2
Apr.09: Coarse-grained simulation of asphaltene-hydrocarbon containing systems
13015
An introduction to some methods to calculate loads and stiffnesses in bolted assemblies
82018 B
The pressure distribution at zero incidence over selected families of blunt axisymmetric forebodies
92035 A
Calculation methods for steadily loaded, off-set pivot, tilting-pad thrust bearings (Guide to use of computer program
A9235)
PERF RG 2/1 B Reduction of take-off and landing measurements to standard conditions
85028 B
Calculation methods for steadily loaded axial groove hydrodynamic journal bearings. Superlaminar operation (To be used
in conjunction with Item No. 84031)
SPD-M10-1
Apr.09: Thermodynamic modelling of asphaltene-oil systems using SAFT
91026 E
Analysis of cam roller followers
SPB-M14-1
Sept.10: Interactions and rheological properties of Asphaltenes studied by Atomic Force Microscopy
SPG-M7-3
Apr.08: Detailed dynamic behaviour of pre-heat train HEXs undergoing fouling
SPF-M6-2
Apr.08: Fluid dynamic gauging
96029 C
Transonic data memorandum VGK method for two-dimensional aerofoil sections Part 2: User manual
SPA-M10-3
Apr.09: Characterisation of Maya crude oil (in terms of mass and structure)
97019 A
Equilibrium temperatures in self-contained bearing assemblies (Use of computer program A9719)
SPA-M10-2
Apr.09: Probing into petroleum heath-exchanger deposits with spectroscopic imaging
96025 F
Drag due to lift for non-planar swept wings up to high angles of attack at subsonic speeds
SPF-M6-1
Apr.08: Annulus flow tests (status report on tube and annulus flow rig development)
PERF EG 8/2 B Estimation of rolling manoeuvrability
07004 A
Flow in rotating components - discs, cylinders and cavities
92034 A
Calculation methods for steadily loaded fixed-inclined-pad thrust bearings (Guide to use of computer program A9234)
90022 D
Force analysis of planar linkages
2010
2010
2010
2010
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2010
2010
2010
2010
ESDU
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0
0
0
0
2010
2010
2010
2010
2010
2010
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2010
ESDU
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ESDU
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ESDU
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ESDU
0
0
0
0
0
0
0
0
0
2010
2010
2010
2010
ESDU
ESDU
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ESDU
0
0
0
0
2010
2010
ESDU
ESDU
0
0
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
ESDU
ESDU
ESDU
ESDU
ESDU
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ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
498
499
500
501
502
503
504
505
506
507
508
509
510
511
512
513
514
515
516
517
518
519
520
521
522
SPD-M6-4
85046 D
SPA-M6-3
95023 A
Apr.08: Asphaltene precipitation from crude oil
Quadrature methods for the evaluation of definite integrals
Apr.08: Questions: Elemental analysis
Dynamics of a simple flexible rotor supported in axial groove hydrodynamic journal bearings (Guide to use of computer
program A9523)
SPE-M12-1
Sept.09: Stirred vessel fouling tests
PERF EG 6/4 C Estimation of ground run during landing
SPB-M6-3
Apr.08: Atomic Force Microscopy (background to technique)
SPG-M7-1
Apr.08: Fouling in crude oil preheat trains. Control and mitigation
00018
Example of statistical analysis of wet runway friction: ground-test machine data
91038 B
Film thickness in lubricated Hertzian point contacts (Use of computer program A9138)
SPD-M6-3
Apr.08: Phase behavior of complex mixtures
90007 B
Procedures for balancing planar linkages using rotating counterweights
13008
Fatigue strength of low-carbon steel stud threads under axial and combined axial and bending loading
PERF EG 8/1 B Estimation of turning performance
SPB-M11-1
Apr.09: Interactions and Rheological Properties of Asphaltenes Investigated using AFM
SPG-M7-2
Apr.08: Fouling mitigation in pre-heat trains. Network simulation
01008 C
Computer program for wind speeds and turbulence properties: flat or hilly sites in terrain with roughness changes
99017 A
Example of statistical analysis of wet runway friction: aircraft with limited set of test data
SPE-M15-1
Sept.10: Stirred vessel fouling tests and research into crude oil fouling
96015 A
Design and material selection for dry rubbing bearings (Use of computer program A9615)
SPA-M10-1
Apr.09: Fouling chemistry
93016 B
Parameter estimation of linear systems from frequency response measurements (Computer program)
79005 A
Undamped natural vibration of shear buildings
91037 B
Film thickness in lubricated Hertzian line contacts (Use of computer program A9137)
SPD-M6-2
Apr.08: Coarse-Grained simulation of asphaltene-hydrocarbon containing systems
SPF-M14-1
Sept.10: Annulus flow tests (status report on tube and annulus flow rig development)
85027 B
Film thicknesses in lubricated Hertzian contacts (EHL). Part 1: two-dimensional contacts (line contacts)
99016 A
Example of statistical analysis of wet runway friction: aircraft with extensive set of test data
82037 E
The response of two-degree-of-freedom systems (computer program)
SPA-M6-2
Apr.08: Advances in characterising h lt bi asphaltenes combining macro- and micro- ATR-FTIR Imaging
94034 A
Dimensions, deflections and stresses for Hertzian contacts under combined normal and tangential loading (Guide to use of
computer program A9434)
74030 B
Characteristics of atmospheric turbulence near the ground Part I: definitions and general information
SPD-M6-1
Apr.08: Thermodynamic modelling of asphaltene-oil systems using SAFT
87011 E
Prediction of single-stream jet noise in flight from static circular-nozzle data
SPG-M15-1
Sept.10: Fouling - Challenges and Opportunities
99015 C
Statistical analysis of wet runway friction for aircraft and ground-test machines
PERF EG 6/2 C Estimation of approach speed
SPB-M6-2
Apr.08: Colloidal Interactions Between Asphaltene and Different Surfaces Measured by Atomic force microscopy (AFM)
SPD-M6-1
Apr.08: Thermodynamic modelling of asphaltene-oil systems using SAFT
TM 151
Stresses in the tread material of an unloaded inflated tyre
2010
2010
2010
2010
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
2010
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
2010
2010
2010
2010
2010
2010
2010
2010
2010
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
523
524
525
526
527
528
529
530
531
532
533
534
535
536
537
538
539
540
541
542
543
544
545
546
547
548
549
550
551
552
553
554
555
556
557
558
559
SPD-M14-1
93006 A
Sept.10: Thermodynamic modelling of asphaltene-oil systems using SAFT
2010
Calculation methods for steadily loaded axial groove hydrodynamic journal bearings. Low viscosity process fluid
2010
lubrication (Guide to use of computer program A9306)
96031 D
Computer programs for response of structures to vortex shedding Structures of circular or polygonal cross section Part 1.
2010
Microsoft Excel module
SPB-M6-1
Apr.08: Interfacial and Rheological Properties of Asphaltenes Investigated using AFM
2010
PERF EG 5/1 C Estimation of take-off distance
2010
SPF-M12-2
Sept.09: Fluid dynamic gauging
2010
69005 A
The response of first- and second-order systems
2009
PERF RP 1/0 A Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers
2009
A2
WIND ENGINEERING SERIES: TITLES Issue 5
2009
CFD-BMK
CFD Benchmarks for predicting friction losses and flow characteristics in straight pipes
2009
09011
PERF RP 2/0 A General method of performance reduction for piston-engined aircraft with constant-speed propellers
2009
06024 B
Dynamic characteristics of cylindrical helical springs. Part 1: deformation, stresses and stability
2009
72021 C
Effect of wing on rolling moment due to yawing
2009
PERF RT 1/3 A Performance reduction for aircraft with turbo-props. â__Non-dimensionalâ__ graphical method. Range and endurance.
2009
TN 08008 A
CFD studies for the validation of friction losses and flow characteristics in circular straight pipes with smooth walls
2009
A1
FLUID MECHANICS, INTERNAL FLOW SERIES:TITLES Issue 6
2009
PERF RT 1/0 B Performance reduction for aircraft with turbo-props. â__Non-dimensionalâ__ graphical method
2009
08012
Aerodynamics and aero-acoustics of rectangular planform cavities. Part IIIB: Alleviation of unsteady flow effects - acoustic 2009
suppression using passive devices
00003
Dynamics Series record of documents
2009
PERF RT 1/1 A Performance reduction for aircraft with turbo-props. â__Non-dimensionalâ__ graphical method. Level speed
2009
CFD-BPG
CFD Best Practice Guidelines for modelling friction losses and flow characteristics in straight pipes
2009
09010
75031 B
Drag of two-dimensional steps and ridges immersed in a turbulent boundary layer for Mach numbers up to 3
2009
00030
Structures series organisation: preface amendment record - Issue 4
2009
04023 B
Aerodynamics and aero-acoustics of rectangular planform cavities Part II: Unsteady flow and aero-acoustics
2009
08006
Example of risk analysis for an aircraft subject to performance errors
2009
00037 D
Aircraft Performance Program Part 7: Error messages Programs APP02 and APP03
2009
00013 A
OSCAM. Computer-aided cam mechanism design: installation Associated software: OSCAM
2009
90020 B
Airframe-induced upwash at subsonic speeds
2009
89013 B
Transverse (through-the-thickness) shear stiffnesses of fibre reinforced composite laminated plates
2009
08007
Strength of lugs under oblique load
2009
08011
Aerodynamics and aero-acoustics of rectangular planform cavities. Part IIIA: Alleviation of unsteady flow effects
2009
Introduction
08015 A
Dynamic characteristics of cylindrical helical springs. Part 2: vibration
2009
00005
Tribology Series record of documents
2009
09003
Dynamic characteristics of cylindrical helical springs. Part 3: impact loading on compression springs
2009
PERF RP 1/2 A Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Rate of climb 2009
82023 B
The estimation of basic dimensions of disc cams with translating followers
2009
PERF RP 1/1 A Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Level speed. 2009
ESDU
ESDU
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0
ESDU
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
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0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
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0
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ESDU
ESDU
ESDU
0
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0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
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0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
560
561
562
563
564
565
566
567
568
569
570
571
572
573
574
575
576
577
578
579
580
581
582
583
584
585
586
587
588
589
590
591
592
593
594
595
596
597
93015 B
Program for calculation of maximum lift coefficient of plain aerofoils and wings at subsonic speeds
09005
Introduction to Damping
PERF RT 1/2 A Performance reduction for aircraft with turbo-props. â__Non-dimensionalâ__ graphical method. Rate of climb
93032 A
Examples of excrescence drag prediction for typical wing components of a subsonic transport aircraft at the cruise
condition
PERF RP 1/3 A Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Final
consumption
99031 B
Computer program for estimation of lift curve to maximum lift for wing-fuselage combinations with high-lift devices at
low speeds
09012
Aerodynamics of parachutes
02008 C
Aerodynamics and aero-acoustics of rectangular planform cavities Part I: Time-averaged flow
09004
Labyrinth seal flow
02007 B
AMOPS: computer program for the calculation of area and moments of area of planar shapes
09013
Initial buckling of flat isosceles triangular plates under compression reacted by compression and/or shear
01001 B
Elasto-plastic buckling of flat isotropic stiffened panels and struts in compression.
SPA-M9-1
Chemical photography of petroleum deposits. Characterisation of asphaltenes and deposited foulants using vibrational
spectroscopy - Sept. 08 update.
SPB-M8-1
Determining the mechanical properties of aspheltene films - Sept. 08 update.
97025 A
Similarity rules for application in aircraft performance work.
90023 D
Airframe noise prediction
SPD-M8-1
Coarse-grained simulation of asphaltene-hydrocarbon containing systems - Sept. 08 update.
STRUSW
Structures Series - Software.
PERF RJ2/0 B Introductory sheet on the analytical method of performance reduction for aircraft with turbo-jets.
03001 A
Elastic buckling of long, flat, symmetrically-laminated (AsBoDf), composite stiffened panels and struts in compression.
87005 D
Increment in aerofoil profile drag coefficient due to the deployment of a single-slotted flap.
66027 F
Friction losses for fully-developed flow in straight pipes.
08014
Guide to contaminated runway testing
82006 B
Selection of DRD cam laws.
PERF RJ1/2 C Performance analysis for aircraft with turbo-jets. "Non-dimensional" graphical method. Rate of climb.
SPD-M8-2
Thermodynamic modelling of asphaltene - oil systems using SAFT - Sept. 08 update.
08010
Example of similarity methods applied to aircraft drag data from flight test
PERFSW
Performance Series - Software. - Issue 8
08003
Treatment of risk within commercial air transport
NOISSW
Aircraft Noise Series - Software.
84041 A
Properties of common engineering materials
MECHSW
Mechanisms Series - Software.
SPF-M8-2
Fluid dynamic gauging - Sept 08 update.
PERF RJ2/1 A Analytical method of performance reduction for aircraft with turbo-jets. Rate of climb.
71011 A
Stresses due to interference-fit pins and bushes in plates, strips or lugs
SPD-M8-3
Predicting adsorption isotherms using a two-dimensional Statistical Associating Fluid Theory.
08004
Example of risk analysis applied to en-route flight path for large jet transport aircraft
06005
Dwell-rise-fall-dwell cam laws. Computer program.
2009
2009
2009
2009
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2009
ESDU
0
2009
ESDU
0
2009
2009
2009
2009
2009
2008
2008
ESDU
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ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
ESDU
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ESDU
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ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
598
599
600
601
602
603
604
605
606
607
608
609
610
611
612
613
614
08005
SPC-M9-1
SPG-M8-1
77022 C
08013
99034
07012
SPF-M8-1
SPE-M8-1
SPA-M9-2
08002
05024 B
98016 B
SPG-M8-2
SPF-M3-7
SPG-M5-3
98005 C
615
05008
616
84017 A
617
618
619
620
SPG-M3-3
74015 A
SPA-M4-2
AERO
A.08.01.05 B
73023 A
87027 A
SPF-M3-6
94044 A
81039 C
77016 B
68002 A
01011 B
77009 B
74021 C
95025 B
SPG-M5-1
86015 B
81043 C
SPD-M2-2
621
622
623
624
625
626
627
628
629
630
631
632
633
634
635
Example of risk analysis applied to aircraft landing distance
Dynamics of fouling deposition and removal in the presence of aging effects - Sept. 08 update.
Advanced modelling and simulation of hot end refinery heat exchangers for fouling mitigation - Sept. 08 update.
Equations for calculation of International Standard Atmosphere and associated off-standard atmospheres
Increment in wing profile drag coefficient due to the deployment of a single-slotted flap.
Transonic Aerodynamics Series organisation: preface, location schedule, amendment record.
Crack growth criteria for the estimation of fatigue life.
Tube and annulus flow loop development and testing - Sept. 08 update.
Stirred vessel fouling tests - Sept. 08 update.
A study of deposit formation in a micro-bomb reactor (MBR): effect of residence time - Sept. 08 update.
Fouling in cooling systems using fresh water.
Flow through sudden contractions of duct area: pressure losses and flow characteristics.
Elastic buckling of flat isotropic stiffened panels and struts in compression.
Fouling mitigation/control in preheat trains - Sept. 08 update.
Developing a high temperature and pressure fluid dynamic gauge for the crude oil annular test section.
Simulating operation of refinery preheat trains subject to fouling.
Design and performance evaluation of heat exchangers: the effectiveness-NTU method. Part 3: graphical and analytical
data. - Incorporates A, B, and C
Cyclic stress-strain response of type 316 austenitic stainless steels during low-cycle fatigue at temperatures between -269
and 800 degrees C (-452 and 1472 degrees F).
Contact phenomena. II: stress fields and failure criteria in concentrated elastic contacts under combined normal and
tangential loading.
Impacts of fouling in oil refineries, standard design methods, proposed approach.
Performance in incompressible flow of plane-walled diffusers with single-plane expansion.
Advances in characterising asphaltenes combining macro- and micro-ATR-FTIR imaging
Aerodynamic centre in two-dimensional flow.
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2007
2007
2007
ESDU
ESDU
ESDU
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ESDU
ESDU
ESDU
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ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
2007
ESDU
0
2007
ESDU
0
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
0
0
0
0
Pressure losses in three-leg pipe junctions: combining flows.
Computer program for the prediction of fluid transients in liquid-filled systems.
Fluid Dynamic Gauging in annular geometries.
Excrescence drag levels on aircraft.
Flow of liquids. Pressure losses across orifice plates, perforated plates and thick orifice plates in ducts.
The gravitational component of pressure gradient for two-phase gas or vapour/liquid flow through straight pipes.
Shafts with interference-fit collars. Part I: some factors affecting the design of an assembly.
Compendium of curves and approximating algebraic functions.
Pressure losses in curved ducts: interaction factors for two bends in series.
The stability and response of linear systems. Part III: methods of analysis based on frequency response.
Drag due to lift for plane swept wings, alone or in combination with a body, up to high angles of attack at subsonic speeds.
Fouling in crude oil preheat trains.
Fluid transients in pipes. Estimation of maximum pressures and forces in steam lines.
Sound in low velocity ventilation ducts.
Molecular modelling of asphaltene containing systems.
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
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ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
636
637
638
639
640
651
652
653
654
655
85009 A
78001 A
73022 A
79037 B
AEROW
01.01.05 E
SPC-M3-1
88025 D
94046 A
86030 A
86032 A
TN 06023 A
83046 A
SPF-M3-4
satexpress
CFD-BPG
07008
SPF-M4-5
83037 D
77029 C
SS3 E
97029 A
656
657
SPF-M3-5
84038 A
658
659
660
661
662
663
664
665
SPF-M4-1
74020 C
72009 A
74040 C
03017 A
06013 A
SPE-M4-1
FMI2 B
666
667
668
SPH-M3-1
SPD-M4-1
05007
669
670
671
SPF-M4-4
SPA-M2-2
88019 D
641
642
643
644
645
646
647
648
649
650
Fluid transients in pipes. Use of air inlet/outlet valves as surge suppression devices.
The momentum-change component of pressure change in two-phase flow and other non-equilibrium effects.
Pressure losses in three-leg pipe junctions: dividing flows.
A guide to fan selection and performance.
Item Nos 72024 and 97020 together provide a more accurate value of and they supersede this Item, which has been
temporarily retained within the Sub-series because it is used within the methods of some other Items.
Fundamental transfer processes.
Derivation of primary air-data parameters for hypersonic flight.
Ejectors and jet pumps: computer program for design and performance for steam/gas flow.
Ejectors and jet pumps. Design for steam driven flow.
Boiling inside tubes: critical heat flux for upward flow in uniformly heated vertical tubes.
CFD validation studies for pressure loss and flow characteristics in sudden contractions.
Fluid transients in pipes and tunnels. Speed of propagation of pressure waves.
CFD studies of fluid mixing in the loop: manifold design.
EXPRESS program. User Guide
CFD Best Practice Guidelines for modelling pressure loss and flow characteristics. Incompressible flow in sudden
contractions.
Fluid Dynamic Gauging (FDG) in duct flows.
Pressure losses in curved ducts: single bends.
Pressure losses in curved ducts: coils.
Guide to Items on struts, beams and shafts.
One-dimensional representation of steady, spatially non-uniform flow. An equivalent mean-value set for compressible
flow. Part 2. Implementation for an ideal, thermally-perfect gas.
Crude oil supplies. Overall progress.
Fluid transients in pipes. Pressure surge following pump trip in rising mains and other similar discharge lines. Suppression
using air vessels.
Sept 07 Overview - Tube and annulus flow tests.
The stability and response of linear systems. Part II: methods of displaying stability characteristics.
Pressure drop in ducts across round-wire gauzes normal to the flow.
Pressure loss during crossflow of fluids with heat transfer over plain tube banks without baffles.
Pitching moment curve of wings with leading-edge and trailing-edge high-lift devices deployed at low speeds.
Propeller slipstream modelling for incidence and sideslip.
Stirred vessel fouling tests.
Guide to the flow relationships and statistical methods used in the Data Items on two-phase flow pressure gradients in
straight pipes.
Technology transfer.
Thermodynamics and molecular modelling.
Strain-life data for type 316 austenitic stainless steels at temperatures between -269 and 816 degrees C (-452 and 1501
degrees F).
CFD studies of fluid mixing in the loop: Manifold design.
Advanced characterisation of asphaltenes using vibrational spectroscopy.
Calculation methods for along-wind loading. Part 3. Response of buildings and plate-like structures to atmospheric
turbulence.
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
2007
2007
ESDU
ESDU
0
0
2007
2007
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
2007
2007
2007
ESDU
ESDU
ESDU
0
0
0
2007
2007
2007
ESDU
ESDU
ESDU
0
0
0
672
673
674
675
676
677
85032 A
66030 C
85044 A
SPA-M4-1
SPB-M4-1
95011 B
678
679
680
681
682
683
68003 C
87015 B
75026 C
STSTSW
SPA-M4-3
82009 D
684
685
686
687
688
689
SPD-M2-1
07011
AERO
W.01.01.05 E
SPG-M3-1
SPF-M3-1
68004 A
690
691
692
693
694
695
696
697
698
699
700
701
702
703
704
705
706
707
708
709
SPD-M4-3
90025 A
07005
SPC-M3-2
SPF-M4-2
82003 A
81021 A
SPB-M2-1
SPG-M3-4
06019
82001 A
VACFSW
84013 B
SPE-M3-1
Fouling
FMI1 A
SPG-M5-2
SPF-M3-2
67035 B
88014 B
Ejectors and jet pumps. Design and performance for incompressible liquid flow.
Pressure losses in flowmetering devices.
Fluid transients in pipes. Pressure surge following booster pump trip. Suppression using pump bypass.
Characterization of asphaltenes and deposited foulants - Overview Sept 07
Interfacial and rheological properties of asphaltenes investigated using AFM
One-dimensional representation of steady, spatially non-uniform flow. An equivalent mean-value set for compressible
flow. Part 1. Implementation for an ideal, calorically-perfect gas.
Shafts with interference-fit collars. Part II: nominal elastic interface pressures and stresses.
Performance improvement of axial diffusers for incompressible flow.
Performance of circular annular diffusers in incompressible flow.
Stress and Strength Series - Software.
Characterisation of asphaltenes and deposited foulants.
Compressible flow of gases. Pressure losses and discharge coefficients of orifice plates, perforated plates and thick orifice
plates in ducts.
Modelling asphaltenes using soft or related approaches.
Damping of structural vibrations by acoustic radiation.
Slope of lift curve for two-dimensional flow. - Incorporates Amendments A, B, C, D, and E
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
2007
2007
2007
ESDU
ESDU
ESDU
0
0
0
Control and mitigation.
Pipe and annulus flow tests.
Shafts with interference-fit collars. Part III: procedure for calculation of nominal elastic interface pressures and stresses in
assemblies of three or more elements.
Coarse grained simulation of asphaltene-hydrocarbon containing systems.
Performance of conical diffusers in subsonic compressible flow.
Normal force and pitching moment of non-axisymmetric bodies: square cross-sections with corner rounding.
Stability of two-fluid flow through a channel.
Major effort on rig design.
Example to illustrate the use of Data Items on noise from ducted ventilation and air-conditioning systems.
Pressure losses caused by obstructions in ducts or pipes.
Interfacial and rheological properties of asphaltenes studied by atomic force microscopy.
Why another HEN simulator?
Temperature measurement: resistance thermometry.
An introduction and guide to noise in ventilation, air-conditioning and other ducting systems.
Vibration and Acoustic Fatigue Series - Software.
Fluid transients in pipes. Reduction and control of pressure surges in liquids.
Stirred vessel fouling tests.
Summary of UK-Government funded research programme into crude oil fouling.
Introductory memorandum on the pressure losses in internal flow systems.
Modelling of shell-and-tube heat exchanger undergoing crude oil fouling.
Major effort on rig design.
Jet flow parameters
Computer program for the prediction of air-lift pump performance.
2007
2007
2007
ESDU
ESDU
ESDU
0
0
0
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
710
711
712
713
714
715
716
717
718
719
720
721
722
723
724
725
726
727
728
729
730
731
732
733
734
735
736
737
738
739
740
741
742
743
744
745
746
747
748
SPF-M4-3
06018
82002 A
SPA-M2-1
89012 A
SPC-M3-3i
77032 C
SPD-M4-2
97002 D
69022 E
SPF-M3-3
76027 B
SPO-M4-1
74028 D
76018 D
CFD-BMK
07009
SPC-M5-1
07010
SPH-M5-1
72011 E
84039 B
89047 C
WINDSW
TRIBSW
02001 A
DYNMSW
TRANSW
06004
05022
06012
06008
06001
85015 B
AERO
F.02.01.06 B
06021
06006
87024 D
FMIFSW
90036 C
Design details.
Temperature measurement: thermocouples.
Reduction of sound in ventilation and similar air distribution systems.
Characterisation of asphaltenes and deposited foulants.
Two-phase flow pressure losses in pipeline fittings. - Reprinted with Amendment A
Modellization of two phase flow with application to aphaltenes deposition and removal.
Fluctuating loads and dynamic response of bodies and structures in fluid flows - background information.
Modelling asphaltenes using SAFT or related approaches.
Information for the use of Data Items on high-lift devices.
Pressure losses in valves.
Preliminary design of the annulus test section.
Introduction to design and performance data for diffusers.
Fouling in a crude oil preheat train - a new attack on an old problem
One-dimensional compressible gas flow in ducts.
The frictional component of pressure gradient for two-phase gas or vapour/liquid flow through straight pipes.
CFD Benchmarks for predicting pressure loss and flow characteristics. Incompressible flow in sudden contractions.
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
Fundamental transfer processes.
Extrapolating wind-tunnel data to full-scale Reynolds number Part 2: Procedures
Sept. 07 Overview - Technology transfer.
Flow through a sudden enlargement of area in a duct.
Strength of angles and club-foot fittings (transmitting tensile loads).
In-plane forces and moments on installed inclined propellers at low forward speeds.
Wind Engineering Series - Software.
Tribology Series - Software.
Viscosity of liquids: Aliphatic nitriles.
Dynamics Series - Software.
Transonic Aerodynamics Series - Software.
Dwell-Rise-Fall-Dwell and Dwell-Fall-Rise-Dwell cam laws. Sections 14 to 23: examples.
Extrapolating wind-tunnel data to full-scale Reynolds number. Part 1: Principles
The influence of propeller slipstream on aircraft rolling moment due to sideslip.
Viscosity of liquids: Branched chain aliphatic esters.
Aerofoil skin friction drag for Mach numbers below the drag-rise condition.
Introduction to installation effects on thrust and drag for propeller-driven aircraft.
Profile drag coefficient increment due to full-span single-slotted flaps (Handley Page and NACA types).
2007
2007
2007
2007
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
Strength of lugs under transverse load.
Viscosity of liquids: Aliphatic alcohols, glycols and glycerol.
Low-speed drag coefficient increment at constant lift due to full-span plain flaps.
Fluid Mechanics, Internal Flow Series - Software.
Structures of non-circular cross section: dynamic response due to vortex shedding.
2006
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
749
06015
750
751
752
753
92006 A
88029 C
03007 A
06016
754
755
756
757
85029 A
92012 A
06014
06020
758
759
760
761
06009
06007
96037 A
02014 A
762
763
764
765
766
767
768
769
06025
FFRASW
FENDSW
00027 A
94025 A
04019 A
74019 C
02013 A
770
771
772
773
774
95019 A
96020 A
97027 A
FMIASW
06003
775
776
777
778
779
780
781
782
00016 B
02012 A
93017 A
67037 A
67036 A
96023 A
97008 A
04007 A
783
784
05015
05001
Full-potential method for three-dimensional wings and wing-body combinations - inviscid flow. Part 3: Method with
improved estimates of body lift and drag contributions (FPIBE).
A background to the handling qualities of aircraft.
Yawing moment coefficient for plain ailerons at subsonic speeds.
Viscosity of liquids: Aromatic compounds containing oxygen.
Full-potential method for three-dimensional wings and wing-body combinations - inviscid flow. Part 4: Evaluation of
trailing-vortex drag and wave components.
Calculation of ground performance in take-off and landing.
Fouling and slagging in combustion plant.
Zero-lift drag coefficient increment due to full-span plain flaps.
Computer program for estimation of aerofoil characteristics at subcritical speeds: lift-curve slope, zero-lift incidence and
pitching moment, aerodynamic centre and drag polar minimum.
Fatigue damage and life under random loading.
Viscosity of liquids: Glycol ethers.
A qualitative introduction to static aeroelasticity: controllability, loads and stability.
Full-potential (FP) method for three-dimensional wings and wing-body combinations - inviscid flow. Part 2: Use of FP and
related programs.
Guide to linear Least Squares curve fitting techniques
Fatigue - Fracture Series - Software.
Fatigue - Endurance Series - Software.
Aerofoil profile drag for Mach numbers below the drag rise condition.
Viscosity of liquids: Aliphatic and cyclic ketones.
Endurance of high-strength steels.
The stability and response of linear systems. Part 1: Introduction.
Full-potential (FP) method for three-dimensional wings and wing-body combinations - inviscid flow. Part 1: Principles and
results.
Viscosity of liquids: Aliphatic ethers.
Viscosity of liquids: Straight chain aliphatic esters.
Viscosity of liquids: Aliphatic amines.
Fluid Mechanics, Internal Flow (Aerospace) Series - Software.
Dwell-Rise-Fall-Dwell and Dwell-Fall-Rise-Dwell cam laws. Sections 9 to 13: segments having asymmetric rise and fall
periods.
Heat exchanger fouling in the pre-heat train of a crude oil distillation unit.
Subsonic base and boat-tail pressure drag of cylindrical bodies with circular-arc boat-tails and a central propulsive jet.
Thermal conductivity of liquids: Carboxylic acids.
Direction and incidence angles.
Geometric and kinematic relationships for various axis systems.
Thermal conductivity of liquids: Branched chain aliphatic esters.
Thermal conductivity of liquids: Aliphatic aldehydes and ketones.
Normal force and pitching moment of non-axisymmetrical bodies: square and triangular cross-sections without corner
rounding.
Normal force and pitching moment of non-circular bodies: elliptical cross-sections at supersonic speeds.
Prediction of combustor noise from gas turbine engines
2006
ESDU
0
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2006
2006
2006
2006
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
2006
2006
2006
2006
2006
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
2005
2005
2005
2005
2005
2005
2005
2005
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
2005
2005
ESDU
ESDU
0
0
785
786
787
788
789
77021 B
96018 A
99010 A
88004 A
94023 A
790
791
792
793
794
795
796
797
798
799
800
801
802
803
804
805
806
807
808
809
810
77021 B
02002 A
67038 B
05020
96012 A
05021
94022 A
84010 A
00021 A
05010
95018 A
99012 A
04012
05004
98018 A
83015 A
99013 B
05003
86002 D
81040 D
89014 D
811
812
813
67007 A
04018
67006 A
814
815
816
67004 A
03014
90034 C
817
818
819
820
821
822
67005 A
04010
04009
97026 B
04005
TM 148
Properties of a standard atmosphere.
2005
Thermal conductivity of liquids: Straight chain aliphatic esters.
2005
Supersonic base drag of cylindrical bodies with a central propulsive jet.
2005
Thermal conductivity of liquids: Mixtures.
2005
Thermal conductivity of liquids: Halogenated aliphatic hydrocarbons. Part 3. Halogenated higher hydrocarbons (C3 to
2005
C16).
Properties of a standard atmosphere.
2005
Thermal conductivity of liquids: Aromatic compounds containing oxygen.
2005
Measures of damping.
2005
Thermal conductivity of liquids: Aliphatic hydrocarbons. Part 1. Alkanes.
2005
Subsonic and transonic base and boat-tail pressure drag of cylindrical bodies with circular-arc boat-tails.
2005
Thermal conductivity of liquids: Aliphatic hydrocarbons. Part 2. Alkenes, dienes and trienes.
2005
Thermal conductivity of liquids: Halogenated aliphatic hydrocarbons. Part 2. Halogenated ethanes.
2005
Thermal conductivity of liquids: Aromatic hydrocarbons.
2005
Thermal conductivity of liquids: Aliphatic nitriles.
2005
Thermal conductivity of liquids: Alicyclic compounds - cycloalkanes, alkenes, alkanols, alkanones and alkylamines.
2005
Thermal conductivity of liquids: Aliphatic ethers.
2005
Thermal conductivity of liquids: Aliphatic diesters.
2005
Examples of construction of carpet plots from experimental data.
2005
Loads in circular frames due to hydrostatic pressure
2005
Thermal conductivity of liquids: Halogenated aromatic hydrocarbons.
2005
Thermal conductivity of liquids: Heterocyclic nitrogen compounds.
2005
Thermal conductivity of liquids: Glycols, glycerol and their aqueous solutions.
2005
Loads in circular frames due to symmetric floor loading.
2005
Drag and pressure recovery characteristics of auxiliary air inlets at subsonic speeds.
2004
The stability and response of linear systems. Part VII: examples.
2004
Normal force, pitching moment and side force of forebody-cylinder combinations for angles of attack up to 90 degrees and 2004
Mach numbers up to 5.
Inertia cross-coupling during a rapid rolling manoevre. Estimation of critical roll rate.
2004
Fatigue - Fracture Mechanics series organisation: preface amendment record
2004
Inertia cross-coupling during a rapid rolling manoeuvre. Theoretical background and discussion of simplified stability
2004
boundaries.
Conversion formulae for rotation and translation of body axes.
2004
Surface flow visualisation in aircraft design
2004
Computer program for the calculation of normal force and pitching moment of forebody-cylinder combinations at angles of 2004
attack up to 90 degrees and Mach numbers up to 5, including the effects of conical boat-tailing.
Introduction to inertia cross-coupling of the lateral and longitudinal motions during a rapid rolling manoeuvre.
2004
Mobilities and impedances of structures. Part 2: Compendium of point mobilities of infinite structures.
2004
Mobilities and impedances of structures. Part 1: Compendium of frequency response functions.
2004
OSMEC. Computer-aided linkage design: User manual.
2004
Non-Newtonian fluids: tube viscometry worked example
2004
The implications of flow property profiles on determination and application of non-dimensional pressure loss coefficients 2004
for flow of incompressible fluids
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
ESDU
ESDU
ESDU
0
0
0
ESDU
ESDU
ESDU
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
823
824
825
826
827
828
829
830
842
843
97023 B
97034 A
96028 B
95012 B
03015
73024 C
87039 B
AERO
F.08.01.01 D
97028 B
76010 B
75020 C
AERO
F.08.01.02 C
97006 A
77007 A
03005
85024 A
80030
97011 A
PD MEMO
0301
89017 B
99011 A
844
845
846
93003 A
90019 C
99005 A
847
848
849
850
851
852
853
854
855
89005 A
03006
97009 A
04008
94032 A
89006 C
67001 A
96003 E
98017 A
856
857
858
859
67003 A
92009 A
95013 A
67002 A
831
832
833
834
835
836
837
838
839
840
841
OSMEC. Computer-aided linkage design: installation.
Non-Newtonian fluids: Guide to classification and characteristics.
VGK method for two-dimensional aerofoil sections. Part 1: Principles and results.
Non-Newtonian fluids: obtaining viscometric data for frictional pressure loss estimation for pipeflow.
Transonic data memorandum. VGK method for two-dimensional aerofoil sections. Part 7: VGK for Windows.
Performance of conical diffusers in incompressible flow.
Parameter estimation of linear systems in the absence of process noise: (i) methods based on the least-squares principle.
Pitching moment coefficient increment due to flaps for unswept wings.
2004
2004
2004
2004
2004
2004
2004
2003
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
Thermophysical properties of sulphur hexafluoride.
Heat capacity and enthalpy of liquids: halogenated methanes.
Estimation of far-field sound pressure levels due to buzz-saw noise of a supersonic fan or compressor.
Increment to C sub m sub zero due to flaps on swept-back wings.
2003
2003
2003
2003
ESDU
ESDU
ESDU
ESDU
0
0
0
0
Selection and costing of heat exchangers. Plate-fin type.
Heat capacity and enthalpy of liquids: halogenated ethanes and ethylenes.
AMOPS: Computer program for the calculation of area and moments of area of planar shapes.
Heat capacity and enthalpy of liquids: organic sulphur compounds (thiols and sulphides).
Radial, mixed and axial flow pumps. Introduction
Wing lift coefficient increment at zero angle of attack due to deployment of plain trailing-edge flaps at low speeds.
The evaluation of vapour-pressure data
2003
2003
2003
2003
2003
2003
2003
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
Thermophysical properties of propan-2-ol (isopropyl alcohol): Part 1. The ideal gas and the saturated liquid and vapour.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: Aliphatic
hydrocarbons - alkanes.
Thermophysical properties of refrigerant R-134a (1,1,1,2-tetrafluoroethane).
Vapour pressures and critical points of liquids. Halogenated ethanes.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: inorganic
gases.
Thermophysical properties of buta-1,3-diene.
Subsonic drag and pressure recovery of rectangular planform flush auxiliary inlets with ducts at angles up to 90 degrees.
Wing lift coefficient increment at zero angle of attack due to deployment of trailing-edge split flaps at low speeds.
Use of Carpet Plots to represent functions of two variables.
Thermophysical properties of R-32 (difluoromethane).
Vapour pressures and critical points of liquids: Halogenated C3 and higher hydrocarbons.
Introduction to notation for aircraft dynamics.
Lift curve of wings with high-lift devices deployed at low speeds.
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge plain flaps at low
speeds.
The equations of motion of a rigid aircraft.
Orthobaric densities and molar volumes of liquids: Halogenated ethanes.
Thermophysical properties of methanol.
Notation for aircraft dynamics.
2003
2003
ESDU
ESDU
0
0
2003
2003
2003
ESDU
ESDU
ESDU
0
0
0
2003
2003
2003
2003
2003
2003
2003
2003
2003
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
2003
2003
2003
2003
ESDU
ESDU
ESDU
ESDU
0
0
0
0
860
98009 A
861
02004 A
862
863
864
99019 A
03004
99004 B
865
866
03011
03008
867
868
869
870
871
872
873
874
875
86007 B
82004 D
88017 B
82032 D
86023 A
94004 A
03010
03016
99014 A
876
877
878
879
880
881
882
883
884
885
83005 A
75015 A
89002 B
97018 B
97024
00029 A
92027 A
81030 A
03005
01013 A
886
887
888
889
03013
02005
98024 A
02003
890
891
82026 E
02010
892
893
894
895
82029 B
82026
94017 A
67033 A
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge split flaps at low
speeds.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: halogenated
hydrocarbons - haloethanes.
Constrained multivariate optimisation techniques for the design of aerofoil sections
Fouling in cooling systems using seawater.
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge single-slotted
flaps at low speeds.
An introduction to lateral static aeroelasticity: controllability, loads and stability.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: Halogenated
hydrocarbons - halopropanes, butanes, ethylenes, benzenes.
Heat capacity and enthalpy of liquids: alkanes.
Thermophysical properties of industrially important fluids on the saturation line: Phenol.
Vapour pressures and critical points of liquids: Organic oxygen compounds.
Thermophysical properties of industrially important fluids on the saturation line: Cresols.
Heat capacity and enthalpy of liquids: alkenes and alkadienes.
Stress analysis of laminated flat plates.
Timing diagrams and their use in mechanism design.
Selection of lubricant class (liquids, solids, semi-solids and gases)
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of trailing-edge double-slotted
and triple-slotted flaps at low speeds.
Thermophysical properties of industrially important fluids on the saturation line: Xylenols.
Heat capacity and enthalpy of liquids: aromatic hydrocarbons.
Thermophysical properties of benzene: Part 1. The ideal gas and the saturated liquid and vapour.
Standard fatigue loading sequences.
Derivation of endurance curves from fatigue test data, including run-outs
Aerofoil and wing pitching moment coefficient at zero angle of attack due to deployment of leading-edge high-lift devices.
Thermophysical properties of nitric oxide.
Heat capacity and enthalpy of liquids: aliphatic ketones.
AMOPS: Computer program for the calculation of area and moments of area of planar shapes.
Aerofoil and wing pitching moment coefficient increment at zero angle of attack due to deployment of leading-edge and
trailing-edge high-lift devices in combination at low speeds.
Thickness selection for the flanges and web of a composite I-section beam subjected to bending and shear.
Flat panels in shear - post-buckling analysis.
Quaternion representation of aeroplane attitude and motion characteristics.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: halogenated
hydrocarbons - halomethanes.
Strong winds in the atmospheric boundary layer. Part 1: hourly-mean wind speeds.
Sound radiation from orthotropic rectangular plates. Part II: validation by comparison with numerical and experimental
results.
Calculation methods for steadily loaded fixed-inclined-pad thrust bearings.
Strong winds in the atmospheric boundary layer. Part 1: hourly-mean wind speeds.
Selection of materials, manufacturing methods and lubricants for cam mechanisms.
General guide to the choice of thrust bearing type.
2003
ESDU
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2003
ESDU
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2003
2003
2003
ESDU
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0
2003
2003
ESDU
ESDU
0
0
2003
2003
2003
2003
2003
2003
2003
2003
2003
ESDU
ESDU
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ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
2003
2003
2003
2003
2003
2003
2003
2003
2003
2003
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
2003
2003
2002
2002
ESDU
ESDU
ESDU
ESDU
0
0
0
0
2002
2002
ESDU
ESDU
0
0
2002
2002
2002
2002
ESDU
ESDU
ESDU
ESDU
0
0
0
0
896
897
898
899
900
901
66032 E
TM 119
02006
65007 A
02015
01024
902
903
904
905
906
908
909
910
911
912
913
914
915
81045 C
01009
84027 C
91024 B
STRUCT
01.01.19 B
STRUCT
01.01.19
85020
90002 C
87030 C
01007
92041 A
01005
98012
01025
916
917
918
919
920
921
922
00053
82020 A
01010
00050
92038 B
85020 G
00051
923
924
00028
00019
925
926
927
01033
00014 A
00052
928
929
930
01012
93018 B
01002
907
Subsonic lift-dependent drag due to boundary layer of plane, symmetrical section wings.
Calculation of planar area and moment properties theoretical background
Temperature measurement: techniques.
General guide to the choice of journal bearing type.
Composites series organisation: preface, amendment record.
Example of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Dual
design point, upper and lower surface shape geometry, leading and trailing edge flap deflections, RAE 2822, Euler code
and BVGK.
Forced convective heat transfer in concentric annuli with turbulent flow.
Condensation of pure fluids in downflow on horizontal integral low-fin tube bundles.
Endurance of fibre-reinforced composite, laminated structural elements subjected to simulated random acoustic loading.
Condensation inside tubes: condensate film coefficient for vertical downflow.
Local buckling and crippling of rectangular tube section struts.
2002
2002
2002
2002
2002
2001
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
2001
2001
2001
2001
2001
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
Local buckling and crippling of rectangular tube section struts.
2001
ESDU
0
Characteristics of atmospheric turbulence near the ground. Part II: single point data for strong winds (neutral atmosphere).
Struts: strength under flexural, local and inter-rivet buckling.
Process integration.
Trailing vortex drag factors for wings with part-span trailing-edge plain flaps.
Stress analysis of single lap bonded joints (adhesive and adherends)
Effect of geometry on low speed pitch-break characteristics of swept wings.
Flexibility of, and load distribution in, multi-bolt lap joints subject to in-plane axial loads.
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design
point: single, upper and lower surfaces geometry and camber line variations, initial aerofoil: NACA 0012 and RAE 2822,
CFD: BVGK.
Viscosity of liquids: Aromatic compounds containing nitrogen.
Introduction to unsteady aerodynamics.
Loading on a rigid aeroplane in steady lateral manoeuvres.
Thermal conductivity of liquids: Aromatic compounds containing nitrogen.
Equivalent lengths of struts (for use in buckling calculations).
Characteristics of atmospheric turbulence near the ground. Part II: single point data for strong winds (neutral atmosphere).
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: hydrocarbons
- alkenes, alkadienes, alkynes, cycloalkanes, aromatics.
Supersonic pressure and Mach number distributions over conical, circular-arc and parabolic boat-tails.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: oxygenated
aliphatic hydrocarbons - alcohols, aldehydes, ketones and ethers.
VGK method for two-dimensional aerofoil sections. Part 6: aerofoil with simple hinged flaps.
OSCAM. Computer-aided cam design: user manual.
Thermal conductivity, viscosity, isobaric specific heat capacity and Prandtl number of gases at low pressure: oxygenated
hydrocarbons - aliphatic esters.
Subsonic pressure drag of boat-tails with negligible annular base area in the presence of a central propulsive jet.
Forced convection heat transfer in straight tubes. Part 2: laminar and transitional flow.
Guide to the use of ESDU Data Items on cam design.
2001
2001
2001
2001
2001
2001
2001
2001
ESDU
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ESDU
ESDU
ESDU
ESDU
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ESDU
0
0
0
0
0
0
0
0
2001
2001
2001
2001
2001
2001
2001
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
2001
2001
ESDU
ESDU
0
0
2001
2001
2001
ESDU
ESDU
ESDU
0
0
0
2001
2001
2001
ESDU
ESDU
ESDU
0
0
0
931
932
933
934
935
936
937
938
939
940
941
942
943
944
945
946
947
948
949
950
951
952
953
954
955
956
957
958
959
960
961
962
963
964
99008
00042
99007
00043
99022
00017
81032 D
00020
00026
87004 B
00023
Orthobaric densities and molar volumes of liquids. Halogenated alkylbenzenes and halogenated styrenes.
EXPRESSplus program. User Guide
Vapour pressures and critical points of liquids: Halogenated alkylbenzenes and halogenated styrenes.
INTEGRITY program for network design. User Guide
Viscosity of liquids: Halogenated aromatic hydrocarbons.
Supersonic base and boat-tail pressure drag of cylindrical bodies with a conical boat-tail and a central propulsive jet
Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds.
Guide to industrial water conservation. Part 1. Water re-use in single contaminant systems.
Supersonic pressure drag of conical, circular-arc and parabolic boat-tails.
Calculation of excrescence drag magnification due to pressure gradients at high subsonic speeds.
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design
point: single, geometry var: LE and TE flaps, initial aerofoil: combat aircraft section, CFD: BVGK (inviscid), Euler code.
98016
Elastic buckling of flat isotropic stiffened panels and struts in compression.
AEROC
RATE OF CHANGE OF LIFT COEFFICIENT WITH CONTROL DEFLECTION IN INCOMPRESSIBLE TWO01.01.03 B
DIMENSIONAL FLOW, (a2)0
AEROC
EFFECT OF NOSE BALANCE ON TWO-DIMENSIONAL CONTROL
04.01.03 B
HINGE-MOMENT COEFFICIENTS
AEROA
STABILITY DERIVATIVE . CONTRIBUTION OF FULL-SPAN DIHEDRAL TO
06.01.03 B
ROLLING MOMENT DUE TO SIDESLIP
00022
Example of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design
point: single, geometry var: LE and TE flaps, initial aerofoil: combat aircraft section, CFD: BVGK (viscous flow)
00041
ENTRANS program. User guide.
86011 B
Numerical methods for the solution of ordinary differential equations: initial value problems.
99003
Generation of GUNACA 23-series of low-drag aerofoils.
99032
VGK method for two-dimensional aerofoil sections. Part 5: design to a specified upper-surface pressure distribution.
72024 D
Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers.
73006 C
Effects of isolated body and wing-body interference on rolling moment due to sideslip: L sub v (with Addendum A for
nacelle effects).
84026 C
Aerofoil maximum lift coefficient for Mach numbers up to 0.4.
99033
Static aeroelasticity: a formal analysis using normal modes.
99001
Geneva mechanisms. Part 4: advanced examples.
84026
Aerofoil maximum lift coefficient for Mach numbers up to 0.4.
82015 A
Fatigue crack propagation rates and threshold stress intensity factor ranges for titanium alloy plate, bar and forgings.
81034 B
Linearised two-dimensional oscillatory airforce coefficients and load distributions on thin aerofoils in subsonic flow.
96035 A
Geneva mechanisms. Part 3: examples.
99020
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design
point: single, geometry variation: LE and TE flap deflection or camber line vars, initial aerofoil: RAE 2822
ME2 C
Design of disc cams with various followers: derivation of kinematic equations.
AERO 00.03.30 Solutions to the oblique shock wave relations for a range of specific heat ratios: pressure coefficient and detachment angle.
A
99021
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design
point: dual, geometry variation: LE and TE flap deflection and camber line vars, initial aerofoil: RAE 2822,
99009
An introduction to Statistical Energy Analysis.
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
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0
0
0
0
0
0
0
0
0
0
0
2000
2000
ESDU
ESDU
0
0
2000
ESDU
0
2000
ESDU
0
2000
ESDU
0
2000
2000
1999
1999
1999
1999
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
1999
1999
1999
1999
1999
1999
1999
1999
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
1999
1999
ESDU
ESDU
0
0
1999
ESDU
0
1999
ESDU
0
965
92002 A
966
95010 C
967
968
969
970
971
972
973
974
975
976
977
978
90030 B
74012 C
73013 B
98021
97007
98023
98001
83042 A
98010
CFA
92036 C
81031 B
979
980
981
982
983
984
985
986
987
988
989
990
991
992
98011
98015
98002
98031
98014
98026
96030 A
98020
98007
CFA
98006
80024 A
79016 B
98004
993
994
995
996
997
998
999
1000
1001
1002
98003
98013
97033
74011 A
97010
97012
97014
88003 D
97003
97013
Lift and rolling moment due to spoilers on wings with trailing-edge flaps deflected at subsonic speeds - extension of Item
No. 90030.
Computer program for estimation of spanwise loading of wings with camber and twist in subsonic attached flow. Liftingsurface theory. (With Appendix A: effect of plain flaps.)
Lift and rolling moment due to spoilers on wings with flaps undeflected at subsonic speeds.
Conversion of lift coefficient increment due to flaps from full span to part span.
Reference frequency of panel with flexible stiffeners.
Viscosity of liquids: Halogenated propanes and higher alkanes.
Heat transfer enhancement in heat exchanger design and utilisation. Part 1. Tube inserts in single-phase flow.
OSMEC. Computer mechanism design: basic examples.
Estimation of airframe skin-friction drag due to impingement of tyre spray.
Estimation of spray patterns generated from the sides of tyres running in water or slush.
Falling film evaporation in vertical tubes.
Conversion factors. - Issue 2
RESPONSE OF STRUCTURES TO ATMOSPHERIC TURBULENCE Computer Programs A9236 and B9236
Fatigue crack propagation rates and threshold stress intensity factor ranges for aluminium alloy plate, extruded bar and
forgings.
Aerofoil incidence for zero lift in subsonic two- dimensional flow.
Orthobaric densities and molar volumes of liquids. Halogenated benzenes.
Thermal conductivity of liquids: Aliphatic amino-alcohols, diamines and nitroalkanes.
VGK method for two-dimensional aerofoil sections. Part 4: estimation of excrescence drag at subsonic speeds.
Vapour pressures and critical points of liquids: Halogenated benzenes.
Example of similarity methods applied to base drag coefficient of conical afterbodies in axisymmetric flow (jet off).
Response of structures to vortex shedding. Structures of circular or polygonal cross section.
Estimation of transmission efficencies of coupled plates
Design and performance evaluation of heat exchangers: the effectiveness-NTU method. Part 5: analytical techniques.
Conversion factors. - Issue 2
Design and performance evaluation of heat exchangers: the effectiveness-NTU method. Part 4: case studies.
Blockage corrections for bluff bodies in confined flows
Inelastic shear stresses and strains in the adhesives bonding lap joints loaded in tension or shear
Design and performance evaluation of heat exchangers: the effectiveness-NTU method. Part 2: performance comparisons
and selection of configurations presented in Part 3.
Design and performance evaluation of heat exchangers: the effectiveness-NTU method. Part 1: introduction.
Aerodynamic principles of winglets.
Methods for analysis of the dynamic response of structures.
Rate of change of lift coefficient with control deflection for full-span plain controls.
Thermal conductivity of liquids: Aliphatic amines.
Vapour pressures and critical points of liquids. Aliphatic and alicyclic amines. I: Primary amines.
Vapour pressures and critical points of liquids. Aliphatic and alicyclic amines. II: Secondary and tertiary amines.
Effect of unshielded and shielded horn balances on hinge moment coefficients for controls at low speeds.
Fuselage interference effects on flap characteristics.
Orthobaric densities and molar volumes of liquids. Aliphatic and alicyclic amines. I: Primary amines.
1999
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1999
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1999
1999
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1998
1998
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1998
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0
0
0
0
0
0
0
1998
1998
1998
1998
1998
1998
1998
1998
1998
1998
1998
1998
1998
1998
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
1998
1998
1997
1997
1997
1997
1997
1997
1997
1997
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
1003
1004
1005
1006
1007
1008
1009
1010
1011
1012
1013
1014
1015
1016
1017
1018
1019
1020
1021
1022
1023
1024
1025
1026
1027
97015
97020
94038 A
96036 A
74009 A
81026 C
97016
97032
97017
97022
96024 A
96034
92020 A
95007
96032
96033
74035 A
ME3
96016
96014
96013
96017
AERO
B.S.02.03.02 C
76033 B
87036 B
1028
1029
96022
80036
1030
1031
1032
1033
1034
1035
77020 A
96021
95024
92024 B
93021 A
94026 A
1036
1037
1038
1039
1040
95008
93034 B
80039 B
80023
76028
Orthobaric densities and molar volumes of liquids. Aliphatic and alicyclic amines. II: Secondary and tertiary amines.
Slope of aerofoil lift curve for subsonic two-dimensional flow.
Computer program for estimation of leading-edge suction distribution for plane thin wings at subsonic speeds.
Design of laminated plates subjected to in-plane loads and bending moments.
Lift coefficient increment at low speeds due to full-span split flaps.
Representation of drag in aircraft performance calculations (with Addenda A to G).
Estimation of airframe drag by summation of components: principles and examples.
Static aeroelasticity: a formal analysis using assumed modes.
Guide to wing aerodynamic design.
Effect of stabilising fins on base drag of cylindrical bodies at supersonic speeds.
Example of statistical techniques applied to analysis of paved runway sizes (Bivariate Normal Distribution).
Thermophysical properties of hydrogen sulphide.
Energy method for analysis of measured airspeed change in landing airborne manoeuvre.
Selection and costing of heat exchangers: plate-and-frame type.
Wing lift coefficient increment at zero angle of attack due to deployment of leading-edge devices at low speeds.
Effect of angle of attack on the base axial force and drag of cylindrical bodies with conical boat-tails.
Subsonic lift-dependent drag due to the trailing vortex wake for wings without camber or twist.
Analysis of Geneva mechanisms: derivation of kinematic and kinetostatic equations.
Vapour pressures and critical points of liquids. Esters of monobasic acids. 1: straight chain alkyl alkanoates.
Fatigue of bolted steel lap joints and doublers.
Fracture toughness (KIc) values for some aluminium alloys.
Orthobaric densities and molar volumes of liquids. Esters of monobasic acids. 1: straight chain alkyl alkanoates.
External wave drag at zero incidence in inviscid flow of simple ducted forebodies and truncated afterbodies.
1997
1997
1997
1997
1997
1997
1997
1997
1997
1997
1996
1996
1996
1996
1996
1996
1996
1996
1996
1996
1996
1996
1996
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
Subsonic base drag of cylindrical bodies with conical boat-tails.
Elastic stresses and deflections for square plates with small initial curvature under uniform pressure on the concave or
convex face.
Orthobaric densities and molar volumes of liquids. Esters of monobasic acids. 2: branched chain alkyl alkanoates.
Introduction to the use of linear elastic fracture mechanics in estimating fatigue crack growth rates and residual strength of
components
Subsonic pressure drag of conical boat-tails.
Vapour pressures and critical points of liquids. Esters of monobasic acids. 2: branched chain alkyl alkanoates.
Example of analysis and representation of static pressure correction data in steady flight.
Aerodynamic centre of wing-body combinations.
Examples of flight path optimisation using a multivariate gradient-search method.
Introduction to the estimation of the lift coefficients at zero angle of attack and at maximum lift for aerofoils with high-lift
devices at low speeds.
Thermal conductivity of liquids: Glycol ethers.
Normal force of low-aspect-ratio cropped-delta wings up to high angles of attack at subsonic speeds.
Elastic adhesive stresses in multistep lap joints loaded in tension
Buckling of rectangular specially orthotropic plates
Lift-interference and blockage corrections for two-dimensional subsonic flow in ventilated and closed wind-tunnels.
1996
1996
ESDU
ESDU
0
0
1996
1996
ESDU
ESDU
0
0
1996
1996
1995
1995
1995
1995
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
1995
1995
1995
1995
1995
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1041
1042
1043
1044
1045
71013
71005
75030 C
95017
94031
1046
95021
1047
1048
1049
1050
1051
93019 A
95020
95015
85027
85001
1052
1053
1054
1055
85031 F
89052
89052 A
95028
1056
1057
1058
1059
1060
1061
1062
1063
1064
91007 D
AERO
F.01.01.09 C
78004 C
90027 A
95002
95014
87003 B
95003
69018 B
1065
1066
1067
71005 D
93024 A
90013 B
1068
1069
1070
1071
93025 A
95004
84018 D
AERO
S.00.03.14 B
95005
95027
93026 A
91014 A
83023 A
1072
1073
1074
1075
1076
Elastic direct stresses and deflections for flat rectangular plates under uniformly distributed normal pressure.
1995
Buckling of flat plates in shear.
1995
Natural frequencies of rectangular flat plates with various edge conditions.
1995
Orthobaric densities and molar volumes of liquids. Aliphatic and aromatic ethers.
1995
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a double- 1995
slotted or triple-slotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
Wing lift coefficient increment at zero angle of attack due to deployment of double-slotted or triple-slotted flaps at low
1995
speeds.
Wing lift increment at zero angle of attack due to deployment of single-slotted flaps at low speeds.
1995
Viscosity of liquids: Carboxylic acids.
1995
Examples of distributions of hard paved runway surface types.
1995
Film thicknesses in lubricated Hertzian contacts (EHL). Part 1: two-dimensional contacts (line contacts)
1995
Elastic stress and strain distributions around circular holes in infinite plates of orthotropic material (applicable to fibre
1995
reinforced composites).
Crack resistance curves.
1995
Construction of inelastic stress-strain curves from minimal materials data (computer program).
1995
Construction of inelastic stress-strain curves from minimal materials data (computer program).
1995
Delamination and free edge stresses in composite laminates subjected to uniform prescribed axial strain and temperature
1995
change.
Lift-curve slope of wing-body combinations.
1995
Lift coefficient increment due to full-span double flap (main flap slotted).
1995
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
ESDU
0
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
0
0
0
0
ESDU
ESDU
0
0
Natural frequencies of thin-walled isotropic, circular-cylindrical shells.
Calculation methods for steadily loaded central circumferential groove hydrodynamic journal bearings.
Vapour pressures and critical points of liquids. Glycols and cyclic diols.
Upwash interference for wings in solid-liner wind tunnels using subsonic linearised-theory.
A method of determining the wave drag and its spanwise distribution on a finite wing in transonic flow.
Orthobaric densities and molar volumes of liquids. Glycols and cyclic diols.
Elastic stresses and deflections for long flat rectangular plates under uniformly distributed and linearly varying normal
pressure.
Buckling of flat plates in shear.
Vortex generators for control of shock-induced separation. Part 1: introduction and aerodynamics.
Normal force and pitching moment of low aspect ratio cropped-delta wings up to high angles of attack at supersonic
speeds.
Vortex generators for control of shock-induced separation. Part 2: guide to use of vane vortex generators.
Vapour pressures and critical points of liquids: Glycol ethers (alkyl cellosolves and carbitols etc.)
Failure analysis of fibre reinforced composite laminates.
Approximate calculation of the pressure changes in two-dimensional supersonic flow.
1995
1995
1995
1995
1995
1995
1995
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
1995
1995
1995
ESDU
ESDU
ESDU
0
0
0
1995
1995
1995
1995
ESDU
ESDU
ESDU
ESDU
0
0
0
0
Orthobaric densities and molar volumes of liquids. Glycol ethers (alkyl cellosolves and carbitols etc.).
Pressure loss and heat transfer for single phase flow in tubes containing twisted tape inserts.
Vortex generators for control of shock-induced separation. Part 3: examples of applications of vortex generators to aircraft.
Maximum lift of wings with trailing-edge flaps at low speeds.
Fracture toughness (K sub I sub c) values of some steels.
1995
1995
1995
1995
1995
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1077
1078
1079
1080
1081
1082
1083
1084
1085
1086
1087
1088
1089
1090
1091
1092
1093
1094
1095
1096
1097
1098
1099
1100
1101
1102
1103
1104
1105
1106
1107
1108
1109
66031 C
Introductory sheet on subcritical lift-dependent drag of wings.
70001 B
Elastic stresses and deflections for flat square plates under uniformly distributed normal pressure.
94012 A
Application of multivariate optimisation techniques to determination of optimum flight trajectories.
AERO
Theoretical properties of two-dimensional supersonic aerofoils of simple section.
W.S.00.03.04 B
95016
Vapour pressures and critical points of liquids. Aliphatic and aromatic ethers.
85001 D
Elastic stress and strain distributions around circular holes in infinite plates of orthotropic material (applicable to fibre
reinforced composites).
94030
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a singleslotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
71013 C
Elastic direct stresses and deflections for flat rectangular plates under uniformly distributed normal pressure.
87013 C
Elastic wrinkling of sandwich columns and beams with unbalanced laminated fibre reinforced face plates (face plates of
AsBoDs, AsBlDs and AsBsDs types).
TD MEMO
A method of estimating drag-rise Mach number for two-dimensional aerofoil sections.
6407 B
95009
Effect of wing height on lift and aerodynamic centre for a slender wing-body combination.
85031 F
Crack resistance curves.
71026 D
Frictional and retarding forces on aircraft tyres. Part II: estimation of braking force.
89052 A
Construction of inelastic stress-strain curves from minimal materials data (computer program).
76028 A
Lift-interference and blockage corrections for two-dimensional subsonic flow in ventilated and closed wind-tunnels.
95006 A
Fatigue life estimation under variable amplitude loading using cumulative damage calculations.
95022
Pitching moment of low-aspect-ratio cropped-delta wings up to high angles of attack at subsonic speeds.
92031 A
Maximum lift of wings with leading-edge devices and trailing-edge flaps deployed.
68032 B
Buckling loads in shear of flat sandwich panels. (Isotropic face plates and corrugated cores, all edges clamped.)
81023 A
Lift and drag of two staggered lifting surfaces at low speeds.
94007
Elastic buckling of cylindrically curved laminated fibre reinforced composite panels with all edges simply-supported under
biaxial loading.
94015
Surface pressure coefficient distributions for axisymmetric forecowls at zero incidence (M sub infinity less than or equal to
1.5).
91012 A
Methods for improving damping. Part 1: an introduction and guide to practical methods of increasing structural damping.
68031 B
Buckling loads under combined longitudinal and transverse direct stress of flat sandwich panels. (Isotropic face plates and
orthotropic cores of zero flexural stiffness, all edges clamped.)
94040
Effects of cabin pressure on climb and descent rates.
94014
Wave drag coefficient for axisymmetric forecowls at zero incidence (M sub infinity less than or equal to 1.5).
94006
Elastic buckling of unbalanced laminated fibre reinforced composite plates. (Rectangular plates of AsBtDs type, all edges
simply-supported under biaxial loading.)
88035 B
Maximum inelastic bending moments and form factors for symmetric bending of beams.
72019 B
Buckling of flat isotropic plates under uniaxial and biaxial loading.
94010
Thermophysical properties of MtBE (methyl tert-butyl ether).
67026 C
Buckling loads in shear of flat sandwich panels. (Isotropic face plates and corrugated cores, all edges simply-supported.)
68033 C
Buckling loads under combined longitudinal and transverse direct stress of flat sandwich panels. (Isotropic face plates and
corrugated cores, all edges clamped.)
67024 C
Buckling loads in shear of flat sandwich panels. (Isotropic face plates and orthotropic cores of zero flexural stiffness, all
edges simply-supported.)
1995
1995
1995
1995
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1995
1995
ESDU
ESDU
0
0
1995
ESDU
0
1995
1995
ESDU
ESDU
0
0
1995
ESDU
0
1995
1995
1995
1995
1995
1995
1995
1995
1994
1994
1994
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
1994
ESDU
0
1994
1994
ESDU
ESDU
0
0
1994
1994
1994
ESDU
ESDU
ESDU
0
0
0
1994
1994
1994
1994
1994
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1994
ESDU
0
1110
1111
81024 A
94033
1112
1113
1114
94039
94009
67025 C
1115
90004 C
1116
1117
1118
1119
88009 B
94005
94013
68030 B
1120
1121
1122
1123
1124
94020
94003
94037
87026 A
AERO
W.00.03.01 B
93011
1125
1126
1127
1128
1129
1130
1131
1132
1133
1134
1135
1136
1137
1138
1139
1140
1141
Drag of axisymmetric cowls at zero incidence for subsonic Mach numbers.
Flat rectangular isotropic plates under uniformly distributed normal pressure. Elastic deflections, stresses and strains,
moments and forces, for various forms of edge restraint.
Effects of small changes on rate of climb.
Symmetric steady manoeuvre loads on rigid aircraft of classical configuration at subsonic speeds.
Buckling loads under combined longitudinal and transverse direct stress of flat sandwich panels. (Isotropic face plates and
orthotropic cores of zero flexural stiffness, all edges simply-supported.)
Maximum inelastic bending moments and end loads in fixed ratio for beam sections of general polygonal shape (computer
program).
Thermophysical properties of toluene. Part I: the ideal gas and the saturated liquid and vapour.
Buckling of flat rectangular orthotropic plates.
NACA 1-series geometry representation for computational fluid dynamics.
Buckling loads in shear of flat sandwich panels. (Isotropic face plates and orthotropic cores of zero flexural stiffness, all
edges clamped.)
Selection of synthetic oils.
Stiffnesses of laminated flat plates.
Leading-edge suction distribution for plane thin wings at subsonic speeds.
Fatigue strength of anodized aluminium alloy.
Critical Mach number for high speed aerofoil sections.
1994
1994
ESDU
ESDU
0
0
1994
1994
1994
ESDU
ESDU
ESDU
0
0
0
1994
ESDU
0
1994
1994
1994
1994
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1994
1994
1994
1994
1994
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
Flat rectangular orthotropic plates under uniformly distributed normal pressure. Elastic stresses and deflections for various
forms of edge restraint.
Pressure distribution on blunt noses of two-dimensional sections at zero incidence in supersonic flow.
1994
ESDU
0
1994
ESDU
0
1994
ESDU
0
1994
ESDU
0
1994
1994
ESDU
ESDU
0
0
1994
1994
ESDU
ESDU
0
0
1994
1994
1994
1994
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1994
1994
1994
ESDU
ESDU
ESDU
0
0
0
1994
1994
ESDU
ESDU
0
0
AERO
W.S.05.03.01 B
AERO
Information on the use of Data Items in the series Wings 02.04.
W.02.04.00 B
94029
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a
trailing-edge split flap, with or without a leading-edge high-lift device, at low speeds.
94002
Orthobaric densities and molar volumes of liquids. Polycyclic phenyl and cyclohexyl compounds.
94024
Thermal conductivity of liquids: Halogenated aliphatic hydrocarbons. Part 4. Halogenated alkenes and alkadienes (C1 to
C4).
94001
Vapour pressures and critical points of liquids. Polycyclic phenyl and cyclohexyl compounds.
94028
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a plain
trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
92013 B
Selection and costing of heat exchangers.
90026 B
Inelastic bending moments, end loads, stresses and strains for beam sections of general polygonal shape.
81047 C
Buckling of flat rectangular plates (isotropic, orthotropic and laminated composite plates and sandwich panels).
94027
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of various
leading-edge high-lift devices at low speeds.
88030 A
Boundaries of linear characteristics of cambered and twisted wings at subcritical Mach numbers.
94005
Buckling of flat rectangular orthotropic plates.
94007
Elastic buckling of cylindrically curved laminated fibre reinforced composite panels with all edges simply-supported under
biaxial loading.
94043
Selection and costing of heat exchangers. Air-cooled type.
94019
Through-the-thickness stresses and failure in the corner radius of a laminated composite section.
1142
1143
94042
94016
1144
AERO
C.04.01.04 C
94041
72019
94021
1145
1146
1147
1148
1149
1150
1151
1152
1153
1154
1155
1156
1157
1158
1159
1160
1161
1162
1163
1164
1165
1166
1167
1168
1169
1170
1171
1172
1173
1174
1175
1176
Selection and costing of heat exchangers. Shell-and-tube type.
Examples of flight path optimisation using a multivariate gradient-search method. Addendum A: variation of optimum
flight profile parameters with range.
Effect of Irving internal balance on hinge-moment coefficient in two-dimensional flow.
Condensation inside tubes: condensate film coefficient in horizontal tubes.
Buckling of flat isotropic plates under uniaxial and biaxial loading.
Thermal conductivity of liquids: Halogenated aliphatic hydrocarbons. Part 1. Halogenated methanes and azeotropic
mixtures.
85007 C
Contact phenomena. III: calculation of individual stress components in concentrated elastic contacts under combined
normal and tangential loading.
94045
Shear force, bending moment and torque of rigid aircraft in symmetric steady manoeuvring flight.
67032 C
Buckling loads under combined longitudinal and transverse direct stress of flat sandwich panels. (Isotropic face plates and
corrugated cores, all edges simply-supported.)
75008 B
Frequencies of vertical and lateral load factors resulting from ground manoeuvres of aircraft.
91019 A
Example of statistical techniques applied to autoland touchdown dispersion (confidence intervals for normal and skew
distributions).
93007
Contribution of body-mounted fins and tailplanes to lateral derivatives due to sideslip at subsonic speeds for general body
width to height ratio.
90006 A
Parameter estimation of linear systems from frequency response measurements.
90024 B
Condensation inside tubes: pressure drop in straight tubes with vertical downflow.
81028 D
Lattice structures. Part 2: mean fluid forces on tower-like space frames.
92023 A
Fatigue propagation behaviour of short cracks in titanium alloys.
93033
Fatigue propagation behaviour of short cracks (1-2 mm) in steels.
93020
Computation of static pressure downstream of a normal shock for hypersonic flight (ambient temperature known).
84030
Longitudinal turbulence intensities over terrain with roughness changes
93008
Thermal conductivity of liquids: Aliphatic alcohols.
91041 B
The statistical analysis of data from Normal distributions, with particular reference to small samples.
93009
Vapour pressures and critical points of liquids: Aliphatic and cyclic ketones.
93023
Example of statistical techniques applied to analysis of effects of small changes.
93010
Orthobaric densities and molar volumes of liquids. Aliphatic and cyclic ketones.
89049 B
Response of structures to atmospheric turbulence. Response to across-wind turbulence components.
89034 A
The maximum lift coefficient of plain wings at subsonic speeds.
91042 A
Normal force of low aspect ratio wing-body combinations up to high angles of attack at supersonic speeds.
91023 A
Condensation inside tubes: pressure drop in straight horizontal tubes.
92029 B
Contribution of ventral fins to sideforce and yawing moment derivatives due to sideslip at low angle of attack.
93012
Viscosity of liquids: Halogenated ethanes.
FAT E.07.01 B Endurance of aluminium alloys (unclad) (in bending).
91031 C
Contribution of fin and tailplane to sideforce and yawing moment derivatives due to sideslip at supersonic speeds at low
angle of attack.
92007 A
Contribution of tailplane-mounted twin fins to sideforce, yawing moment and rolling moment derivatives due to sideslip at
subsonic speeds.
85036 B
Conversion of air-data system pressure errors into height and speed corrections.
93029
Orthobaric densities and molar volumes of liquids. Fused ring compounds.
1994
1994
ESDU
ESDU
0
0
1994
ESDU
0
1994
1994
1994
ESDU
ESDU
ESDU
0
0
0
1994
ESDU
0
1994
1994
ESDU
ESDU
0
0
1994
1993
ESDU
ESDU
0
0
1993
ESDU
0
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
1993
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
1993
ESDU
0
1993
1993
ESDU
ESDU
0
0
1177
82010 C
1178
1179
1180
1181
1182
1183
1184
1185
1186
1187
1188
1189
1190
88007 A
92030 A
93027
92003 A
91027 A
AERO
F.02.01.07 C
93014
70016 B
93028
92018
87033 C
92017
92021
1191
1192
1193
1194
1195
92008
90035 A
92019
69026 B
83018 A
1196
1197
1198
1199
92016
92001
92015
83017 A
1200
1201
1202
1203
1204
1205
1206
92028
92044
86006 A
92043
92026
68021 C
89033 A
1207
1208
1209
1210
1211
1212
1213
83029 D
68046 D
92015
92017
92038
92040
92039
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to sideslip, (Y sub v) sub F, (N sub v)
sub F, (L sub v) sub F, in the presence of body, wing and tailplane.
Effect of environment on fatigue crack propagation in aluminium alloy sheet and plate.
Fatigue propagation behaviour of short cracks in aluminium alloys.
Methods of testing for endurance of structural elements using simulated acoustic loading.
Forced convection heat transfer in straight tubes. Part 1: turbulent flow.
Non-destructive examination - choice of methods.
Conversion factor for profile drag increment for part-span flaps.
1993
ESDU
0
1993
1993
1993
1993
1993
1993
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
Condensation inside tubes. Computer program for pressure drop in straight tubes (horizontal and vertical with downflow). 1993
Terms and notation for fatigue endurance data.
1993
Vapour pressures and critical points of liquids. Fused ring compounds.
1993
Orthobaric densities and molar volumes of liquids. Halogenated ethylenes.
1992
Normal force and pitching moment of conical boat-tails.
1992
Fatigue strength of cruciform and other fillet welded joints in aluminium alloys.
1992
Example of statistical techniques applied to analysis of landing ground roll distance measurements. (Linear regression,
1992
correlation coefficient and F test.)
Direct prediction of a separation boundary for aerofoils using a viscous-coupled calculation method.
1992
Frictional and retarding forces on aircraft tyres. Part V: estimation of fluid drag forces.
1992
Estimation of rate of climb.
1992
Airspeed data for performance calculations.
1992
Axial pressure coefficient distributions for spherically blunted secant ogive forebodies of fineness ratio 1.0, 1.5 and 2.0 at 1992
zero incidence in transonic flow.
Reducing torque fluctuation in linkage drive shafts.
1992
Methods for improving damping. Part 3: damping material data.
1992
Guide to the effect of shot peening on fatigue strength.
1992
The wave drag coefficient of spherically blunted secant ogive forebodies of fineness ratio 1.0, 1.5, and 2.0 at zero incidence 1992
in transonic flow.
Viscosity of liquids: Halogenated methanes.
1992
Analogue to digital transformation.
1992
Pitot and static errors in steady level flight.
1992
Pitching moment of low aspect ratio wing-body combinations up to high angles of attack at supersonic speeds.
1992
Calculation methods for externally pressurised (hydrostatic) journal bearings with capillary restrictor control.
1992
Foredrag of spherically-blunted conical forebodies at zero incidence in supersonic flow for Mach numbers up to 5.
1992
Pressure drag and lift contributions for blunted forebodies of fineness ratio 2.0 in transonic flow (M sub infinity less than or 1992
equal to 1.4).
The correction of flight-test anemometric data.
1992
Atmospheric data for performance calculations.
1992
Guide to the effect of shot peening on fatigue strength.
1992
Fatigue strength of cruciform and other fillet welded joints in aluminium alloys.
1992
Equivalent lengths of struts (for use in buckling calculations).
1992
An introduction to the statistical analysis of engineering data.
1992
Drag due to gaps round undeflected trailing-edge controls and flaps at subsonic speeds.
1992
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
1214
83010 A
1215
1216
1217
1218
1219
1220
87038 B
88013 B
86037 A
86016 A
perfcor B
92022
1221
1222
1223
1224
1225
1226
1227
1228
1229
1230
1231
1232
1233
1234
1235
1236
1237
1238
1239
92040
81046 A
69026 B
78008 C
76016
91039
91006
91034
91003
84031 A
91035
91018
91039
91022
91008
88032
91040
91020
88015 A
1240
1241
1242
1243
1244
1245
1246
1247
87001 B
91021
91022
88032 A
91011
89051 A
82008 B
91029
1248
1249
91015
91016
1250
1251
91032
90005 B
Oscillatory aerodynamics of slender bodies (ASSOCIATED SOFTWARE: ESDUPAC A8310 AVAILABLE THROUGH
SUBSCRIPTION ONLY)
Calibration of anemometric pressure systems for lag.
Rolling moment derivative, L sub xi, for plain ailerons at subsonic speeds.
An introduction to the Z-transform and its application to sampled-data systems.
Frictional and retarding forces on aircraft tyres. Part IV: estimation of effects of yaw.
Corrigenda
Example of statistical techniques applied to analysis of measurements of the landing airborne manoeuvre. (Multiple linear
regression with two independent variables and one dependent variable.)
An introduction to the statistical analysis of engineering data.
Acceleration factors for climb and descent rates at constant EAS, CAS, M.
Airspeed data for performance calculations.
Physical properties of design atmospheres
Generalisation of smooth continuous stress-strain curves for metallic materials
Static and fatigue strength of butt welded joints in aluminium alloys.
Vapour pressures and critical points of liquids. Halogenated ethylenes.
Orthobaric densities and molar volumes of liquids. Halogenated methanes.
Delamination of tapered composites.
Calculation methods for steadily loaded axial groove hydrodynamic journal bearings.
Vapour pressures and critical points of liquids. Alkyl amides.
Example of statistical techniques applied to cruise performance guarantees (Students "t" distribution).
Static and fatigue strength of butt welded joints in aluminium alloys.
Thermophysical properties of nitrous oxide.
Strength of lugs under axial load
Wrinkling of sandwich panel face plates (isotropic face plates on orthotropic cores, in-plane loading or bending).
Thermophysical properties of carbon monoxide.
Variability of standard aircraft performance parameters.
Elastic wrinkling of sandwich panels with laminated fibre reinforced face plates (face plates of AsBoDs, AsBlDs and
AsBsDs types).
Wing pitching moment at zero lift at subcritical Mach numbers.
A method of estimating a flow breakdown boundary for aerofoils and swept wings in transonic flow.
Thermophysical properties of nitrous oxide.
Wrinkling of sandwich panel face plates (isotropic face plates on orthotropic cores, in-plane loading or bending).
Boiling inside tubes: saturated wet-wall heat transfer with mixtures.
Fatigue crack propagation rates for titanium alloy sheets.
Elastic stresses and deflections of helical compression and tension springs of round wire.
Excrescence drag magnification factors at the drag-rise condition for aerofoils with a specified form of upper-surface
pressure distribution.
Fatigue crack propagation rates of experimental aluminium lithium sheet and plate alloys.
Energy height method for flight path optimisation. Addendum A: numerical method suitable for rapid use on IBM PC
compatible computers.
Estimation of airborne performance in landing.
Frequencies of resonance in wind tunnels with ventilated walls and plenum chamber.
1992
ESDU
0
1992
1992
1992
1992
1992
1992
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
1992
1992
1992
1992
1991
1991
1991
1991
1991
1991
1991
1991
1991
1991
1991
1991
1991
1991
1991
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
1991
1991
1991
1991
1991
1991
1991
1991
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
1991
1991
ESDU
ESDU
0
0
1991
1991
ESDU
ESDU
0
0
1252
1253
86031 A
91028
1254
86010 E
1255
1256
84007 A
72017 A
1257
1258
1259
1260
1261
1262
1263
1264
1265
1273
90001
90017
90003
89041 A
90018
77028 F
72016 C
90033
STRUCT
01.01.08 C
89028 A
TM 71
STRUCT
01.01.01 C
SS1 E
90015 A
90031
STRUCT
02.01.08 C
89008 C
1274
1275
1276
1277
1278
81020 A
90012
90028
89020 A
76002 A
1279
1280
1281
1282
1283
90009
89019 A
90002
SS1
STRUCT
01.01.01
STRUCT
01.01.08
1266
1267
1268
1269
1270
1271
1272
1284
Introduction to air data system parameters, errors and calibration laws.
Simplified method for the prediction of aerofoil excrescence drag magnification factor for turbulent boundary layers at
subcritical Mach numbers.
Characteristics of atmospheric turbulence near the ground. Part III: variations in space and time for strong winds (neutral
atmosphere). - Incorporates A, B, C, D, and E
The treatment of calibrations of total air temperature probes for use in flight-test analysis work.
Stress response of flat or singly-curved sandwich panels with cores of zero flexural stiffness subjected to random acoustic
loading.
Boiling inside tubes: post dry-out heat transfer in vertical tubes.
Thermophysical properties of refrigerant R-22 (chlorodifluoromethane).
Thermophysical properties of sulphur dioxide.
Estimation of subsonic far-field jet-mixing noise from single-stream circular nozzles.
Fatigue of aluminium alloy joints with various fastener systems. High load transfer.
Geometrical characteristics of typical bodies.
Natural frequencies of flat or singly-curved sandwich panels with cores of zero flexural stiffness.
Process integration: process change and batch processes.
Local instability of struts with flat sides.
1991
1991
ESDU
ESDU
0
0
1991
ESDU
0
1991
1990
ESDU
ESDU
0
0
1990
1990
1990
1990
1990
1990
1990
1990
1990
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
A procedure for force-balancing planar linkages using counterweights.
A Rayleigh-Ritz method of analysis for vibration of orthotropic plates under static in-plane loading (including shear)
The strength of struts.
1990
1990
1990
ESDU
ESDU
ESDU
0
0
0
Guide to the use of the Stress and Strength Series.
Vapour pressures and critical points of liquids. Halogenated methanes.
Fretting fatigue.
Buckling in compression of sheet between rivets.
1990
1990
1990
1990
ESDU
ESDU
ESDU
ESDU
0
0
0
0
Normal-force-curve and pitching-moment-curve slopes of forebody-cylinder combinations at zero angle of attack for Mach 1990
numbers up to 5.
A method of estimating a separation boundary for two-dimensional aerofoil sections in transonic flow.
1990
Energy height method for flight path optimisation.
1990
Effect of environment on fatigue crack propagation rate in titanium alloy sheet and plate.
1990
Thermophysical properties of isopropyl alcohol. Part II: thermodynamic properties at elevated pressures.
1990
First-order method for estimating the subcritical pressure distribution on a two-dimensional aerofoil in compressible
1990
viscous flow.
Fatigue of aluminium alloy joints with various fastener systems. Medium load transfer.
1990
Orthobaric densities and molar volumes of liquids. Aromatic hydrocarbons.
1990
Struts: strength under flexural, local and inter-rivet buckling.
1990
Guide to the use of the Stress and Strength Series.
1990
The strength of struts.
1990
ESDU
0
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
Local instability of struts with flat sides.
ESDU
0
1990
1285
1286
1287
1288
1289
1290
1291
1292
1293
1294
1295
1296
1297
1298
1299
1300
1301
1302
1303
1304
1305
1306
1307
1308
1309
1310
1311
1312
1313
1314
1315
1316
1317
1318
1319
1320
STRUCT
02.01.08
90008
78021
89046
89031
AERO
C.04.01.08 B
89004
89018
89045
AERO
C.04.01.06 B
89003
89044
AERO
C.04.01.03 B
89001
89015
86038 A
STRUCT
02.03.24
CFS
89007
89032
88001 A
89021
89048
CFS
74037 B
89007
89022
89037
89023
84005 A
89027
AERO
C.04.01.01 B
88010 A
AERO
C.04.01.02 B
89043
89038
Buckling in compression of sheet between rivets.
1990
ESDU
0
Introduction to transonic aerodynamics of aerofoils and wings.
Guide to Items on the strength and stability of struts
Fatigue of aluminium alloy joints with various fastener systems. Low load transfer.
Guide to the selection of surface treatments for the improvement of fatigue strength of steels.
Control hinge-moment coefficient derivative due to tab.
1990
1990
1989
1989
1989
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
Effect of fretting on fatigue strength of aluminium alloys.
Orthobaric densities and molar volumes of liquids. Introduction to Data Items issued after July 1989.
Film thicknesses in lubricated Hertzian contacts. Part 2: point contacts.
Full-span control hinge-moment coefficient derivatives for unswept wings in incompressible flow with allowance for
spanwise variation of sectional properties.
Thermophysical properties of benzene. Part II: thermodynamic properties at elevated pressures.
Friction in bearings.
Effect of nose balance on two-dimensional control hinge-moment coefficients.
1989
1989
1989
1989
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1989
1989
1989
ESDU
ESDU
ESDU
0
0
0
Application of process integration to utilities, combined heat and power and heat pumps.
Introduction to Data Items on flight path optimisation.
Fouling of heat exchanger surfaces: general principles.
Strength of castellations in shear.
1989
1989
1989
1989
ESDU
ESDU
ESDU
ESDU
0
0
0
0
Conversion factors
Flexural and torsional-flexural buckling of thin-walled open section struts.
Parameter estimation of linear systems in the presence of process noise using the Maximum Likelihood method.
Boiling inside tubes: critical heat flux for flow in uniformly heated horizontal tubes.
Information on the use of Data Items on hot structures.
Elastic stress concentration factors. Geometric discontinuities in rods and tubes of isotropic materials.
Conversion factors
Introduction and guide to ESDU data on acoustic fatigue.
Flexural and torsional-flexural buckling of thin-walled open section struts.
Heat transfer definitions and equations.
Orthobaric densities and molar volumes of liquids. Alcohols.
Temperatures in plates subjected to a recovery temperature varying linearly with time.
Estimation of drag due to inoperative turbo-jet and turbo-fan engines using Data Item Nos 81009 and 84004.
Steady state temperatures and thermal stresses in a spherical or cylindrical laminated shell.
Rate of change of hinge-moment coefficient with incidence for a plain control in incompressible two-dimensional flow, (b
sub 1) sub zero.
Thermophysical properties of toluene. Part II: thermodynamic properties at elevated pressures.
Rate of change of hinge-moment coefficient with control deflection for a plain control in incompressible two-dimensional
flow, (b sub 2) sub zero.
A comparison of techniques for balancing planar linkages.
Reflux condensation in vertical tubes.
1989
1989
1989
1989
1989
1989
1989
1989
1989
1989
1989
1989
1989
1989
1989
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
1989
1989
ESDU
ESDU
0
0
1989
1989
ESDU
ESDU
0
0
1321
89024
1322
1323
1324
88006 A
89009
STRUCT
02.03.24 B
89026
AERO
C.04.01.00 C
89039
69023 D
89010
89025
88008
88034
88020
85041 A
88039
88024
83034 A
1325
1326
1327
1328
1329
1330
1331
1332
1333
1334
1335
1336
1337
1338
1339
1340
1341
1342
1343
1344
88018
88005
84016 B
AERO
A.06.01.09 B
88016 A
84035 A
68020 C
1345
1346
1347
1348
1349
1350
1351
88027
88012
87037 A
88011
88028
86022 A
83034
1352
68020 C
1353
1354
1355
1356
67019
87018
87017
87016 A
Resultant forces and moments in completely restrained plates subjected to a recovery temperature varying linearly with
time.
Estimation of drag arising from asymmetry in thrust or airframe configuration.
Hinge moment coefficient derivatives for trailing-edge controls on wings at subsonic speeds.
Strength of castellations in shear.
1989
ESDU
0
1989
1989
1989
ESDU
ESDU
ESDU
0
0
0
Temperatures in plates subjected to a sudden increase in recovery temperature.
Introduction to Data Items on control hinge moments.
1989
1989
ESDU
ESDU
0
0
Boiling inside tubes: pressure drop in straight tubes with upward or horizontal flow.
Average gust frequencies. Subsonic transport aircraft.
Example of procedure in calculation of control hinge moments.
Thermal stresses in unrestrained plates subjected to a recovery temperature varying linearly with time.
Fatigue limit of unnotched steels (related to tensile strength).
Avoidance of buckling of some engineering elements (struts, plates and gussets).
Thermophysical properties of propylene oxide.
Boiling inside tubes: general aspects and saturated wet-wall heat transfer.
The Kalman filter.
Fouling in cooling water systems.
Elastic local buckling stresses of thin-walled unstiffened circular cylinders under combined axial compression and internal
pressure.
Selection of alloys for hydrodynamic bearings.
Vapour pressures and critical points of liquids. C1 to C6 alkanols.
Low-fin staggered tube banks: heat transfer and pressure loss for turbulent single-phase crossflow.
Stability derivative (L sub v) sub gamma. Contribution of part-span dihedral to rolling moment due to sideslip.
1989
1989
1989
1989
1988
1988
1988
1988
1988
1988
1988
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
1988
1988
1988
1988
ESDU
ESDU
ESDU
ESDU
0
0
0
0
Thermophysical properties of ethylene oxide.
Drag of stub wings and fairings on a flat plate with a turbulent boundary layer at subsonic and supersonic speeds.
The compressible two-dimensional turbulent boundary layer, both with and without heat transfer, on a smooth flat plate,
with application to wedges, cylinders, and cones.
Effect of fretting on fatigue strength of titanium alloys.
Vapour pressures and critical points of liquids. C7 to C20 alkanols.
Take-off performance of vectored-jet-thrust V/STOL aircraft.
Parameter estimation of linear systems in the absence of process noise: (ii) the Maximum Likelihood method.
Flow induced acoustic resonance in tubular heat exchangers.
High-fin staggered tube banks: heat transfer and pressure drop for turbulent single phase gas flow.
Elastic local buckling stresses of thin-walled unstiffened circular cylinders under combined axial compression and internal
pressure.
The compressible two-dimensional turbulent boundary layer, both with and without heat transfer, on a smooth flat plate,
with application to wedges, cylinders, and cones.
Static strength of screwed fasteners
Example of take-off field length calculations for a civil transport aeroplane.
Orthobaric densities and molar volumes of liquids. Part 2A: C2 to C16 alkenes.
Effect of size on fatigue strength of steel components.
1988
1988
1988
ESDU
ESDU
ESDU
0
0
0
1988
1988
1988
1988
1988
1988
1988
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
1988
ESDU
0
1988
1987
1987
1987
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1357
1358
1359
86013
81017 A
71019 A
1360
1361
1362
1363
1364
1365
1366
1367
1368
1369
1370
1371
1372
1373
1374
1375
1376
1377
1378
87019
87022
74036 B
87007
72003 A
83024 A
74026 A
87012
87028
87009
87010 A
86013 A
AERO
A.S.06.03.04 B
86012
86033
85016 A
82025 A
86028
86008
1379
1380
1381
1382
86027
86005
86025
86004
1383
1384
1385
1386
1387
1388
1389
83014 A
86017
82030 F
86040
86001
86041
86003
1390
80025
1391
1392
73004
85006
Guide to the use of Data Items on the fatigue strength of welded joints in steels.
Mean forces, pressures, and moments for circular cylindrical structures: finite-length cylinders in uniform and shear flow.
Drag-rise Mach number of aerofoils having a specified form of upper-surface pressure distribution: charts and comments
on design.
Flow induced vibration in tube bundles with particular reference to shell and tube heat exchangers.
Orthobaric densities and molar volumes of liquids. Part 2B: alkadienes and alkynes.
Drag due to a circular cavity in a plate with a turbulent boundary layer at subsonic, transonic and supersonic speeds.
Design and material selection for dry rubbing bearings.
Natural frequencies of built-up, flat, periodic skin-stringer structures. Part I: stringers rigid in bending.
Approximation to the roots of the lateral equations of motion of an aircraft with and without a simple yaw damper.
Estimation of r.m.s. stress in internal plates of a box structure subjected to random acoustic loading.
An introduction to aircraft buffet and buffeting.
Melting points, boiling points and critical properties.
Reliable data sources for key industrial chemicals.
Orthobaric densities and molar volumes of liquids. Part 1A: C1 to C18 alkanes.
Guide to the use of Data Items on the fatigue strength of welded joints in steels.
Spanwise centre of pressure of isolated lifting surface at supersonic speeds.
1987
1987
1987
ESDU
ESDU
ESDU
0
0
0
1987
1987
1987
1987
1987
1987
1987
1987
1987
1987
1987
1987
1987
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
Vapour pressure and critical points of liquids. Part 3A: C6 to C10 alkylbenzenes.
The effect of electrodeposited chromium on the fatigue strength of low alloy steel.
Vapour pressures and critical points of liquids. Part 2B: C7 to C16 alkenes.
Failure modes of fibre reinforced laminates.
Fatigue strength of keyed assemblies.
Calculation methods for steadily loaded axial groove hydrodynamic journal bearings. Low viscosity process fluid
lubrication. (To be used in conjunction with Items Nos. 84031 and 85028.)
Vapour pressure and critical points of liquids. Part 3B: additional alkyl- and alkenylbenzenes.
Vertical deflection characteristics of aircraft tyres.
Design against fatigue: vibration of structures under acoustic or aerodynamic excitation.
Simplified forms of performance equations. Addendum A: effect on aeroplane level speed of small changes in thrust, drag,
weight, power.
Failure criteria for an individual layer of a fibre reinforced composite laminate under in-plane loading.
Propeller/body interaction for thrust and drag.
Fire hazard properties: flash points, flammability limits and autoignition temperatures.
Selection of surface treatments and coatings for combating wear of load-bearing surfaces.
Vapour pressures and critical points of liquids. Part 2C: alkadienes and alkynes.
Conversion of stability derivatives for a general change of body axes.
Example of the use of Data Item No. 85001. Choice of reinforcement for a circular hole in a fibre reinforced laminated
plate. (Data relating to one particular set of laminate properties.)
Mean forces, pressures and flow field velocities for circular cylindrical structures: single cylinder with two-dimensional
flow
Criteria of yielding for ductile materials under static loading
Contribution of wing dihedral to sideforce, yawing moment and rolling moment derivatives due to rate of roll at subsonic
speeds, (Y sub p) sub gamma, (N sub p) sub gamma and (L sub p) sub gamma.
1986
1986
1986
1986
1986
1986
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
1986
1986
1986
1986
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1986
1986
1986
1986
1986
1986
1986
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
1986
ESDU
0
1985
1985
ESDU
ESDU
0
0
1393
1394
1395
1396
1397
1398
1399
1400
85022
85045
85019
85014
85008
AERO
W.01.01.07 B
85026
85010
1401
1402
1403
85013 A
85030
83006 A
1404
1405
1406
1407
1408
1409
1410
1411
1412
1413
1414
1415
1416
1417
1418
84023 A
76011 A
84025 A
85017
85002
85014
84040
84021
84006
STRUCT
02.01.47 A
84022
81009 A
84028
81042 A
TM 49
1419
1420
1421
1422
1423
1424
1425
1426
84009
83038 A
81025 A
84042
72015 B
84020
84004 A
84037
1427
84002
1428
83033 A
Practical guide to the selection of condensers.
1985
Stress concentrations: interaction and stress decay for selected cases.
1985
Fatigue crack propagation rates and threshold stress intensity factors in high strength low alloy steel plate, bar and forgings. 1985
Design for minimum weight. Struts of uniform section. Thin-walled round tubes.
1985
Vapour pressures and critical points of liquids. Part 2A: C2 to C6 alkenes.
1985
Maximum lift coefficients for aerofoil sections at Mach numbers from 0.60. to 0.75.
1985
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
Servomechanism transfer functions.
1985
Estimation of sideforce, yawing moment and rolling moment derivatives due to rate of roll for complete aircraft at subsonic 1985
speeds.
Design of disc cams and their followers: examples.
1985
Force and moment components for take-off and landing calculations.
1985
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of roll, (Y sub p) sub F, (N sub 1985
p) sub F, (L sub p) sub F, in the presence of body, wing and tailplane.
Shell-and-tube exchangers: pressure drop and heat transfer in shellside downflow condensation.
1985
First approximation to take-off field length of multi-engined transport aeroplanes.
1985
Endurance of aluminium alloy lugs with steel interference-fit pins or bushes.
1985
Thrust and drag accounting for propeller/airframe interaction.
1985
Vapour pressures and critical points of liquids. Part 1C: C10 to C24 alkanes.
1985
Design for minimum weight. Struts of uniform section. Thin-walled round tubes.
1985
First approximation to landing field length for civil transport aeroplanes (50 ft, 15.24 m screen).
1984
Vapour pressures and critical points of liquids. Introduction to Data Items issued after September 1984.
1984
Elastic buckling of thin-walled unstiffened circular cylinders under bending, axial compression and internal pressure.
1984
Buckling stress coefficients for parallelogram shaped panels in continuous flat sheet under uniform compression.
1984
ESDU
ESDU
0
0
ESDU
ESDU
ESDU
0
0
0
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
Vapour pressures and critical points of liquids. Part 1A: C1 to C7 alkanes.
Estimation of windmilling drag and airflow of turbo-jet and turbo-fan engines.
Vapour pressures and critical points of liquids. Part 1B: C8 and C9 alkanes.
Vapour pressures and critical points of liquids. XX: additional derivatives of phenol.
CONTRIBUTION TO ROLLING MOMENT DERIVATIVE DUE TO SIDESLIP RESULTING FROM
INTERFERENCE EFFECT OF FIN ON TAILPLANE, (Lv)TH
Nonlinear systems: an introduction to Describing Functions.
Baffled shell-and-tube heat exchangers; flow distribution, pressure drop and heat transfer coefficient on the shellside.
Vapour pressures and critical points of liquids. XIX: phenol and derivatives.
Stiffness data for finite element calculations. Equivalent stiffness factors for shear webs.
Endurance of aluminium alloy structural elements subjected to simulated acoustic loading.
An introduction to time-dependent aerodynamics of aircraft response, gusts and active controls.
Estimation of spillage drag for a wide range of axisymmetric intakes at M less than 1.
Fatigue strength of external and internal steel screw threads under axial loading. (Standard forms not greater than 1.0 inch
diameter.)
Estimation of sideforce, yawing moment and rolling moment derivatives due to rate of yaw for complete aircraft at
subsonic speeds.
Stress intensity factors for corner cracks in loaded holes in lugs and wide plates.
1984
1984
1984
1984
1984
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1984
1984
1984
1984
1984
1984
1984
1984
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
1984
ESDU
0
1984
ESDU
0
1429
1430
1431
1432
1433
1434
1435
1436
1437
1438
1439
1440
1441
1442
1443
1444
1445
1446
1447
1448
1449
1450
1451
1452
1453
1454
1455
1456
1457
1458
1459
1460
1461
82016 A
82034 A
66013 A
84001
84042
84009
84006
STRUCT
02.01.47
84012
79032
84032
83028
83012
77014
83036
83043
83044
83007
STRUCT
03.06.05 A
83027
83043
STRUCT
02.01.22 A
STRUCT
03.06.04 A
83026
83041
STRUCT
02.01.22
STRUCT
02.03.02
STRUCT
00.07.00
STRUCT
00.07.01
STRUCT
00.07.04
83030
STRUCT
00.07.00 A
82017 A
Vapour pressures and critical points of liquids. XXI: cyclic hydrocarbons.
Aircraft forces due to interference between a jet efflux and a slotted flap.
Definitions of terms for acoustic fatigue analysis.
Growth of cracks under constant amplitude fatigue loading: example calculations.
Stiffness data for finite element calculations. Equivalent stiffness factors for shear webs.
Nonlinear systems: an introduction to Describing Functions.
Elastic buckling of thin-walled unstiffened circular cylinders under bending, axial compression and internal pressure.
Buckling stress coefficients for parallelogram shaped panels in continuous flat sheet under uniform compression.
1984
1984
1984
1984
1984
1984
1984
1984
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
Buckling of thin-walled unstiffened circular cylinders under torsion and pressure.
1984
Stress concentrations at grooves for retaining rings or seals (with notes on design against fatigue).
1984
Nonlinear systems: the Describing Function method for closed-loop system response.
1984
Approximate parametric method for propeller thrust estimation. Addendum A: application to fixed-pitch propellers.
1983
Fatigue strength of cold-rolled titanium alloy screw threads under axial load (room temperature and elevated temperatures). 1983
Flat panels in shear Post-buckling analysis
1983
Natural frequencies of rectangular, specially orthotropic laminated plates
1983
Flexible circular frames supported by a shell. Moments, forces and displacements due to concentrated loads and couples.
1983
Plasticity correction factors for plate buckling
1983
Fatigue crack propagation rates and threshold stress intensity factor ranges for aluminium alloy sheet.
1983
Bending moment in elliptical frames due to internal pressure.
1983
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
The synthesis of cam motion by blending segments.
Flexible circular frames supported by a shell. Moments, forces and displacements due to concentrated loads and couples.
Buckling stress coefficients for flat rectangular plates in compression. (Edges restrained against rotation - antisymmetric
rotation.)
Radial deflections of circular frame due to concentrated loads and couples.
1983
1983
1983
ESDU
ESDU
ESDU
0
0
0
1983
ESDU
0
Contribution of body to yawing moment and sideforce derivatives due to rate of yaw, (N sub r) sub B and (Y sub r) sub B.
A summary of the concepts relating to random processes.
Buckling stress coefficients for flat rectangular plates in compression. (Edges restrained against rotation - antisymmetric
rotation.)
Flat panels in shear. Buckling of long panels with transverse stiffeners.
1983
1983
1983
ESDU
ESDU
ESDU
0
0
0
1983
ESDU
0
Information on the use of Data Sheets in the 00.07 series.
1983
ESDU
0
Torsion and secondary warping constants for a bulb angle.
1983
ESDU
0
Primary warping constant for Z-sections with bulbs.
1983
ESDU
0
Selection of filter rating for lubrication systems.
Information on the use of Data Sheets in the 00.07 series.
1983
1983
ESDU
ESDU
0
0
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub 1983
r) sub F, (L sub r) sub F.
ESDU
0
1462
1463
1464
1465
1466
1467
1468
1469
1470
1471
1472
1473
1474
1475
1476
1477
1478
1479
1480
1481
1482
1483
1484
1485
1486
1487
1488
1489
1490
AERO
Profile drag coefficients for two-dimensional biconvex aerofoil with zero heat transfer at supersonic speeds.
W.S.02.04.13 A
STRUCT
Torsion and secondary warping constants for a bulb angle.
00.07.01 A
AERO
Skin friction drag coefficients for a flat plate in two-dimensional flow with zero heat transfer.
W.S.02.04.12 A
82021 A
Pressure loss and heat transfer for single-phase turbulent flow in roughened channels: methods of calculation.
STRUCT
Primary warping constant for Z-sections with bulbs.
00.07.04 A
83031
Dynamic sealing of fluids. II: guide to selection of reciprocating seals.
83001 A
Approximate parametric method for propeller thrust estimation.
73007 A
Stiffness of loaded flat strips under sinusoidally distributed bending couples at their edges (for use in local buckling
calculations). (Uniaxial or biaxial loading. Isotropic or orthotropic materials.)
74038 A
Effect of an axial compressive mean stress on the fatigue strength of aluminium alloy bar (plain and notched).
STRUCT
Flat panels in shear. Buckling of long panels with transverse stiffeners.
02.03.02 B
83007
Fatigue crack propagation rates and threshold stress intensity factor ranges for aluminium alloy sheet.
TD MEMO
Method for the rapid estimation of theoretical spanwise loading due to a change of incidence.
6403 C
STRUCT
Shear forces in circular frame due to concentrated loads and couples.
03.06.03 A
83008
The estimation of basic dimensions of disc cams with swinging followers.
83025
Drag of circular cylinders normal to a flat plate with a turbulent boundary layer for Mach numbers up to 3.
83021
The kinematic design of epicyclic gear trains.
83004
Calculation methods for steadily loaded, off-set pivot, tilting-pad thrust bearings.
STRUCT
Diffusion of loads into flat uniform panels.
02.05.00 A
81038 C
Heat pipes - performance of two-phase closed thermosyphons.
81008 A
The stability and response of linear systems. Part VI: selection of an assessment method.
AERO
Stability derivative L sub p. Effect of fuselage interference on rolling moment due to rolling at supersonic speeds.
A.S.06.03.02 A
AERO
Stability derivative L sub p. Rolling moment due to rolling for radial multi-planar wing arrangements at supersonic speeds.
A.S.06.03.03 A
82024
A guide to the selection of cam and follower type.
AERO 00.01.06 Thermodynamic properties of air in dissociation equilibrium.
A
AERO
Theoretical lift-dependent drag of wings at supersonic speeds.
W.S.02.03.02 B
82028
Pressure drag of spherically-blunted conical forebodies at zero incidence for Mach numbers of 3 and above.
AERO 00.01.08 Specific heat capacities and their ratio as functions of temperature for several common gases.
A
AERO
Conditions behind oblique shock waves for air in dissociation equilibrium.
S.00.03.23 A
AERO
Introductory Item on two-dimensional aerofoils at supersonic speeds.
W.S.00.03.03 A
1983
ESDU
0
1983
ESDU
0
1983
ESDU
0
1983
1983
ESDU
ESDU
0
0
1983
1983
1983
ESDU
ESDU
ESDU
0
0
0
1983
1983
ESDU
ESDU
0
0
1983
1983
ESDU
ESDU
0
0
1983
ESDU
0
1983
1983
1983
1983
1983
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1983
1982
1982
ESDU
ESDU
ESDU
0
0
0
1982
ESDU
0
1982
1982
ESDU
ESDU
0
0
1982
ESDU
0
1982
1982
ESDU
ESDU
0
0
1982
ESDU
0
1982
ESDU
0
1491
1492
1493
1494
1495
1496
1497
1498
1499
1500
1501
1502
1503
1504
1505
1506
1507
1508
1509
1510
1511
1512
1513
1514
1515
1516
1517
1518
1519
1520
STRUCT
02.01.17 A
AERO
S.00.03.22 A
81037 A
Nomogram for strength of stringers in panel in compression.
1982
ESDU
0
Conditions behind normal shock waves in air in dissociation equilibrium.
1982
ESDU
0
Designing with rolling bearings. Part 2: selection of single row angular contact ball, tapered roller and spherical roller
bearings.
Linearised two-dimensional oscillatory airforce coefficients and load distributions on thin aerofoils in supersonic flow.
Notes on the design of helical compression and tension springs of round wire.
Stability derivative L sub p, rolling moment due to rolling for wings at supersonic speeds.
1982
ESDU
0
1982
1982
1982
ESDU
ESDU
ESDU
0
0
0
1982
ESDU
0
1982
ESDU
0
1982
ESDU
0
1982
ESDU
0
1982
1982
1982
1982
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1982
ESDU
0
1982
1982
ESDU
ESDU
0
0
1982
ESDU
0
1982
ESDU
0
1982
ESDU
0
1982
1982
1982
1982
1982
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1982
1982
1982
1982
1982
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
82005 A
83003
AERO
A.S.06.03.01 A
AERO
Properties of plane steady shock waves.
S.00.03.09 A
AERO
Simple-wave flow.
S.00.03.08 A
AERO
Optimum area distribution and associated theoretical transonic drag-rise for aircraft at zero lift.
A.02.03.02 A
AERO
Lift-curve slope for single fin and rudder. (i) Body shape merging into fin.
C.01.01.01 B
81019
Methods for estimating the pressure distribution on a two-dimensional aerofoil in viscous transonic flow.
83002
Allowable stresses for helical compression and tension springs of round wire.
81006 A
Stress concentration factors. Axially loaded lugs with clearance-fit pins.
Notation and
Notation and units in Peformance Data Items
Units
AERO
Lift-curve slope of isolated lifting surface at supersonic speeds.
A.S.01.03.02 A
81033 A
Atlas of performance curves for crank-rocker and slider-crank linkages.
STRUCT
Nomogram for strength of stringers in panel in compression.
02.01.17
AERO 00.01.11 Mollier chart of the thermodynamic properties of argon-free air in dissociation equilibrium: T = 2 000 K to T = 13 000 K.
A
AERO
The calculation of the theoretical characteristics of two-dimensional aerofoils at supersonic speeds.
W.S.00.03.05 A
81013 A
Effect of trailing-edge flaps on sideforce and yawing moment derivatives due to sideslip, (Y sub v) sub f and (N sub v) sub
f.
81027 A
Lattice structures. Part 1: mean fluid forces on single and multiple plane frames.
ME1 B
Guide to the use of Item No. 76005. Kinematic and dynamic data for crank-rocker and slider-crank linkages.
70023 A
The measurement and analysis of climb and excess power performance.
82013
Laminate stacking sequences for special orthotropy. (Application to fibre reinforced composites).
AERO 00.01.12 Mollier chart of the thermodynamic properties of argon-free air in dissociation equilibrium: T = 100 K to T = 6 000 K.
A
73019 C
Approximate methods for estimation of cruise range and endurance: aeroplanes with turbo-jet and turbo-fan engines.
81006
Stress concentration factors. Axially loaded lugs with clearance-fit pins.
78023
Fatigue strength of transverse welded joints and attachments in steels under bending loading.
82014
Designing with rolling bearings. Part 3: special types.
82033
First approximation to take-off distance to 50 ft (15.2 m) for light and general aviation aeroplanes.
1521
1522
1523
1524
1525
1526
1527
1528
1529
1530
1531
1532
1533
1534
1535
1536
1537
1538
1539
1540
1541
1542
1543
1544
1545
1546
1547
1548
1549
AERO
Wave drag of flat plates with blunt noses at zero incidence.
W.S.02.03.10 A
AERO
Pitching velocity derivatives for wings at supersonic speeds Z sub q and M sub q.
W.S.08.03.02 B
77002 A
Design of parallel axis straight spur and helical gears: geometric design.
81016
Viscosity of liquid aromatic hydrocarbons.
81007
Fatigue strength in bending of steel I-beams with welded attachments
80020
Average downwash at the tailplane at low angles of attack and subsonic speeds
AERO
Kinetic pressure in the wake behind a wing.
W.05.01.01 A
81044
Heat transfer coefficients for water or steam in plain circular tubes: fully-developed turbulent flow.
AERO
Aerodynamic heating: temperatures at a perfectly insulated surface neglecting radiation.
W.S.00.03.18 B
81035
An introduction to aircraft noise lateral attenuation.
AERO
One-dimensional isentropic gas flow.
S.00.03.07 A
AERO
Stability derivative L sub p, rolling moment due to rolling for swept and tapered wings.
A.06.01.01 A
66028 A
Relationships between some common intake parameters.
81010
Thermophysical properties of industrially important fluids on the saturation line: ammonia.
81041
Flexibilities of and stresses in thin unpressurised pipe bends with flanged ends under in-plane bending: influence of bend
angle.
AERO 00.02.05 Heat transfer under conditions of forced convection for the subsonic turbulent flow of gases in smooth straight ducts of
A
constant cross section.
AERO
Flow field of subsonic axisymmetric jet in a parallel stream.
A.08.01.09 A
AERO
Introductory notes on the drag at zero incidence of bodies at supersonic speeds.
B.S.02.03.01 C
69007 B
The determination of gross thrust and mass flow in flight. (Air breathing ducted-flow engines with convergent nozzles.)
69006 A
Introduction to the measurement of thrust in flight. (Air breathing ducted-flow engines.)
81022
Guide to the use of Data Items in the design of bonded joints.
AERO
Effect of gap on the slope of lift curve and slope of lift increment curve due to control surface deflection.
C.01.01.04 A
68037 A
Local instability of bonded corrugated-core sandwich panels under longitudinal compression. (Symmetrical cores with
identical face plates.)
68029 A
Information on the use of Data Items on sandwich panels.
STRUCT
Initial buckling of flat plates under bending and compression or tension.
02.04.04 A
STRUCT
Flexural properties of stringer sections (lipped and unlipped angles, channels and Z-sections).
01.00.01 A
71004 B
Flange efficiency factors for curved beams under bending in the plane of curvature.
AERO
Pressure distribution on forebodies and afterbodies of revolution at zero incidence in inviscid flow.
B.S.05.03.01 A
STRUCT
Shear centre of D-section.
00.06.05 A
1982
ESDU
0
1982
ESDU
0
1981
1981
1981
1981
1981
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
1981
1981
ESDU
ESDU
0
0
1981
1981
ESDU
ESDU
0
0
1981
ESDU
0
1981
1981
1981
ESDU
ESDU
ESDU
0
0
0
1981
ESDU
0
1981
ESDU
0
1981
ESDU
0
1981
1981
1981
1980
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1980
ESDU
0
1980
1980
ESDU
ESDU
0
0
1980
ESDU
0
1980
1980
ESDU
ESDU
0
0
1980
ESDU
0
1550
1551
1552
1553
1554
1555
1556
1557
1558
1559
1560
1561
1562
1563
1564
1565
1566
1567
1568
1569
1570
1571
1572
1573
1574
1575
1576
1577
1578
AERO
Forebody-afterbody interference wave drag of simple pointed or ducted body shapes with short midbodies.
B.S.02.03.08 A
STRUCT
Information on the use of Data Items in the Struct 00.06. series.
00.06.00 A
73018 A
Introduction to estimation of range and endurance.
77019 A
Vapour pressures and critical points of liquids. XI: heterocyclic nitrogen compounds.
STRUCT
Method of calculating stress distribution in a reinforced symmetrical shell under bending.
00.06.01 A
80035
Buckling of outstanding flanges. Direct stresses varying linearly or parabolically
71004
Flange efficiency factors for curved beams under bending in the plane of curvature.
STRUCT
Shear centre of circular arc section.
00.06.04 A
STRUCT
Initial buckling of flat plates under bending and compression or tension.
02.04.04
STRUCT
Flexural properties of stringer sections (lipped and unlipped angles, channels and Z-sections).
01.00.01
SS3
Guide to Items on struts, beams and shafts.
STRUCT
Buckling stress coefficients for flat rectangular plates tapered in thickness, under compression.
02.01.49
STRUCT
Buckling stress coefficients for slightly curved plates with clamped edges.
02.01.10
STRUCT
Buckling stress coefficients for curved plates in shear (circumferential length exceeding axial length, edges simply02.03.19
supported).
AERO
Examples in the use of the Mollier chart (isentropic flow and Prandtl-Meyer expansion for air in dissociation equilibrium).
S.00.03.27 A
79008
Elastic stress concentration factors. Rectangular notch in the edge of a wide flat plate in tension.
AERO
Supersonic base pressure of cylindrical bodies.
B.S.02.03.12 A
77017 B
Endurance of titanium alloy lugs (Ti-6Al-4V, annealed and Ti-4Al-4Mo-2Sn-0.5Si).
77024 B
Thermal conductivity, viscosity, heat capacity, density and Prandtl number of sea water and its concentrates.
77031 A
Heat transfer by free convection and radiation - simply shaped bodies in air and other fluids.
STRUCT
Buckling stress coefficients for flat rectangular plates tapered in thickness, under compression.
02.01.49 A
STRUCT
Buckling stress coefficients for slightly curved plates with clamped edges.
02.01.10 A
STRUCT
Buckling stress coefficients for curved plates in shear (circumferential length exceeding axial length, edges simply02.03.19 B
supported).
STRUCT
Average and edge stresses for slightly curved plates with clamped edges in compression with initial irregularities.
02.01.11 B
AERO 00.03.28 Conditions behind normal shock waves in a perfect gas for various values of gamma.
A
AERO
Rate of change of lift coefficient with control deflection in incompressible two-dimensional flow, (a sub 2) sub zero.
C.01.01.03 B
66018 A
The relation between sound pressure level and r.m.s. fluctuating pressure.
66017 A
Combination of levels in dB.
68023
Thermal conductivity, viscosity, heat capacity, density and Prandtl number of solid, liquid and gaseous heavy water.
1980
ESDU
0
1980
ESDU
0
1980
1980
1980
ESDU
ESDU
ESDU
0
0
0
1980
1980
1980
ESDU
ESDU
ESDU
0
0
0
1980
ESDU
0
1980
ESDU
0
1980
1979
ESDU
ESDU
0
0
1979
ESDU
0
1979
ESDU
0
1979
ESDU
0
1979
1979
ESDU
ESDU
0
0
1979
1979
1979
1979
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1979
ESDU
0
1979
ESDU
0
1978
ESDU
0
1978
ESDU
0
1978
ESDU
0
1978
1978
1978
ESDU
ESDU
ESDU
0
0
0
1579
1580
1581
1582
1583
1584
1585
1586
1587
1588
1589
1590
1591
1592
1593
1594
1595
1596
1597
1598
1599
1600
1601
1602
1603
1604
1605
1606
1607
1608
1609
AERO
S.00.03.06 C
72012 B
66016 A
STRUCT
01.01.10 B
71016 C
68008 C
77018 A
CF2
68010 C
78030
78020
77018
78016
72012
STRUCT
02.01.11
STRUCT
01.01.10
STRUCT
02.01.02
STRUCT
02.01.03
STRUCT
02.01.16
STRUCT
02.01.23
STRUCT
02.01.24
STRUCT
02.03.18
77023
77030
77011
FAT E.05.06 A
FAT E.05.01 A
STRUCT
02.01.24 A
77001
77033
STRUCT
02.01.23 A
Introductory sheet on isentropic flow and shock waves.
1978
ESDU
0
Information on the use of Data Items on the buckling of plates and compression panels manufactured from isotropic
materials.
Bandwidth correction.
Torsional instability of stringers and struts of angle section.
1978
ESDU
0
1978
1978
ESDU
ESDU
0
0
Fluid forces, pressures and moments on rectangular blocks.
Specific heat capacity at constant pressure of ice, water and steam.
Curved panels in shear. Post-buckling analysis. - Includes Amendment A: 10/1977
Conversion factors for fluid flows.
Density of ice, water and steam.
Struts with lateral loads.
Local buckling and crippling of I, Z and channel section struts
Curved panels in shear. Post-buckling analysis. - Includes Amendment A: 10/1977
The effect of post-weld treatments on fatigue at fillet welded attachments
Information on the use of Data Items on the buckling of plates and compression panels manufactured from isotropic
materials.
Average and edge stresses for slightly curved plates with clamped edges in compression with initial irregularities.
1978
1978
1978
1978
1978
1978
1978
1978
1978
1978
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
1978
ESDU
0
Torsional instability of stringers and struts of angle section.
1978
ESDU
0
Average and edge stresses for long flat plates in compression for different edge conditions.
1977
ESDU
0
Average and edge stresses for thin flat aluminium alloy plates in compression.
1977
ESDU
0
Strength of stringers in panel in compression.
1977
ESDU
0
Average and edge stresses in long flat rectangular plates in compression under varying edge conditions.
1977
ESDU
0
Stiffness after buckling. Flat rectangular plates in compression. (Edges simply-supported.)
1977
ESDU
0
Buckling stress coefficients for curved plates in shear (axial length exceeding circumferential length, edges simplysupported).
Shear centre and primary warping constant for lipped and unlipped channel and Z-sections.
Buckling of struts. Lipped and unlipped Z sections.
Fatigue strength of transverse butt welds in steel plate under axial loading
Endurance of bonded lap joints. (Aluminium alloy sheet material; phenolic resin/vinyl powder glue, tensile loading.)
Endurance of structural joints. (Aluminium alloy material - tensile loading.)
Stiffness after buckling. Flat rectangular plates in compression. (Edges simply-supported.)
1977
ESDU
0
1977
1977
1977
1977
1977
1977
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
Effect of intake total pressure loss on net thrust at take-off: turbo-jet and turbo-fan engines.
Fatigue of wrought and cast annealed Ti-5Al-2.5Sn titanium alloy. (In bending and under axial loading.)
Average and edge stresses in long flat rectangular plates in compression under varying edge conditions.
1977
1977
1977
ESDU
ESDU
ESDU
0
0
0
1610
1611
1612
1613
1614
1615
1616
1617
1618
1619
1620
1621
1622
1623
1624
1625
1626
1627
1628
1629
1630
1631
1632
1633
1634
1635
1636
1637
1638
1639
1640
1641
74018 A
Lost range, fuel and time due to climb and descent: aircraft with turbo-jet and turbo-fan engines.
STRUCT
Average and edge stresses for long flat plates in compression for different edge conditions.
02.01.02 A
FAT E.05.07 A Endurance of bonded double strap joints. (Aluminium alloy sheet material; phenolic resin/vinyl powder glue, tensile
loading.)
77003
Elastic stresses and deflections under uniform pressure of flat rectangular sandwich panels; all edges clamped (isotropic
face plates and orthotropic cores of zero flexural stiffness).
73026 A
Introduction to non-dimensional methods for the measurement of performance of turbine-engined helicopters.
STRUCT
Average and edge stresses for thin flat aluminium alloy plates in compression.
02.01.03 A
77023
Shear centre and primary warping constant for lipped and unlipped channel and Z-sections.
73027 A
Non-dimensional methods for the measurement of hover performance of turbine-engined helicopters.
STRUCT
Strength of stringers in panel in compression.
02.01.16 A
77030
Buckling of struts. Lipped and unlipped Z sections.
77015
Lost range, fuel and time due to climb and descent: propeller-driven aeroplanes.
AERO
Pitot and static tubes in supersonic flow.
S.00.03.15 B
76026 A
Lift and drag due to spoiler operation in the ground run.
77027
Fatigue of wrought and cast Ti-6Al-4V titanium alloy. (In bending and under axial loading.)
STRUCT
Buckling stress coefficients for curved plates in shear (axial length exceeding circumferential length, edges simply02.03.18 A
supported).
STRUCT
Inter-rivet buckling curves for specific materials.
02.01.09 B
74003 A
Normal incidence absorption coefficients and acoustic impedances of typical single layer fibrous lining materials.
76008
Drag of transverse rows of spherically-headed rivets immersed in a turbulent boundary layer at subsonic and supersonic
speeds.
74022 A
Buckling of corrugated shear webs.
74004 A
Normal incidence absorption coefficients and acoustic impedances of single layer perforated sheet liners.
STRUCT
Moments in circular frame due to concentrated loads and couples.
03.06.01 A
TM 19
Effects of truncation on diffuser performance
66006 A
Design for minimum weight. Struts of uniform section. Thin-walled square tubes.
STRUCT
Direct forces in circular frame due to concentrated loads and couples.
03.06.02 A
76030
Thermal conductivity of carbon dioxide gas and liquid.
71014 A
Local buckling of compression panels with flanged stringers.
66007 A
Design for minimum weight. Struts of uniform section. I-sections.
76013
Elastic stresses and deflections under uniform pressure of flat rectangular sandwich panels; all edges simply-supported
(isotropic face plates and orthotropic cores of zero flexural stiffness).
71023 A
Normal melting points, boiling points and critical points of n-alkyl aldehydes and ketones.
76023
Buckling of struts. Lipped and unlipped channel sections.
76005
Kinematic and dynamic data for crank-rocker and slider-crank linkages. (Mechanisms Workbench.)
STRUCT
Collapse coefficients for unstiffened circular cylinders under uniform external pressure.
04.09.01 A
1977
1977
ESDU
ESDU
0
0
1977
ESDU
0
1977
ESDU
0
1977
1977
ESDU
ESDU
0
0
1977
1977
1977
ESDU
ESDU
ESDU
0
0
0
1977
1977
1977
ESDU
ESDU
ESDU
0
0
0
1977
1977
1977
ESDU
ESDU
ESDU
0
0
0
1976
ESDU
0
1976
1976
ESDU
ESDU
0
0
1976
1976
1976
ESDU
ESDU
ESDU
0
0
0
1976
1976
1976
ESDU
ESDU
ESDU
0
0
0
1976
1976
1976
1976
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1976
1976
1976
1976
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1642
76022
1643
STRUCT
02.04.01 A
76021
73025 A
75006 A
76034
75005 A
70003 A
STRUCT
01.01.24 A
70007 A
76032
76023
71014
74022
76013
1644
1645
1646
1647
1648
1649
1650
1651
1652
1653
1654
1655
1656
1657
1658
1659
1660
1661
1662
1663
1664
1665
1666
1667
1668
1669
1670
1671
1672
1673
1674
1675
1676
76007
75006
70003
66006
STRUCT
02.04.01
STRUCT
02.01.09
STRUCT
01.01.24
69015
75007
75016
75034
75035
75034
75007
75033
AERO
S.00.03.13 B
AERO
A.S.02.03.01 B
75014
75035
69015 A
Elastic stresses and deflections under uniform pressure of flat rectangular sandwich panels; long edges clamped, short
edges simply-supported (isotropic face plates and orthotropic cores of zero flexural stiffness).
Buckling stress ratios for plates under uniform compression and shear.
1976
ESDU
0
1976
ESDU
0
Dynamic viscosity of carbon dioxide gas and liquid.
Stresses in the core of a sandwich panel under local normal loading.
Design for maximum structural efficiency. Isotropic sandwich panels under uniaxial compression.
Estimation of take-off thrust using generalised data for turbo-jet and turbo-fan engines.
Performance data for the critical operation of nominally two-dimensional double-ramp supersonic intakes.
Local buckling of compression panels with unflanged integral stiffeners.
The compressive instability of hydraulic jacks.
1976
1976
1976
1976
1976
1976
1976
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
Design for minimum weight. Compression panels with unflanged integral stiffeners having dimensional restrictions.
Fatigue strength of longitudinal flange-to-web welds in steel I-beams and T-sections
Buckling of struts. Lipped and unlipped channel sections.
Local buckling of compression panels with flanged stringers.
Buckling of corrugated shear webs.
Elastic stresses and deflections under uniform pressure of flat rectangular sandwich panels; all edges simply-supported
(isotropic face plates and orthotropic cores of zero flexural stiffness).
Fatigue strength of longitudinal fillet welded attachments and joints in steels under axial loading
Design for maximum structural efficiency. Isotropic sandwich panels under uniaxial compression.
Local buckling of compression panels with unflanged integral stiffeners.
Design for minimum weight. Struts of uniform section. Thin-walled square tubes.
Buckling stress ratios for plates under uniform compression and shear.
1976
1976
1976
1976
1976
1976
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
1976
1976
1976
1976
1976
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
Inter-rivet buckling curves for specific materials.
1976
ESDU
0
The compressive instability of hydraulic jacks.
1976
ESDU
0
Solar heating. Total direct irradiance within the Earths atmosphere.
Geometric stress concentration factors: two adjacent unreinforced circular holes in infinite flat plates.
Fatigue strength of transverse fillet and cruciform butt welds in steels
Initial buckling stress, maximum direct stress and shear strain of square plates in shear with central circular holes.
Initial buckling of square plates in shear with central flanged circular holes.
Initial buckling stress, maximum direct stress and shear strain of square plates in shear with central circular holes.
Geometric stress concentration factors: two adjacent unreinforced circular holes in infinite flat plates.
Elastic stress concentration factors. Double radius fillets in shouldered shafts in torsion.
Inviscid supersonic flow past cones at zero incidence: (ii) surface pressure coefficient and shock angle for circular cones.
1975
1975
1975
1975
1975
1975
1975
1975
1975
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
Explanatory notes on transonic and supersonic area rules.
1975
ESDU
0
Flexibilities of and stresses in thin pipe bends under in-plane bending: influence of bend angle and tangent pipe ends.
Initial buckling of square plates in shear with central flanged circular holes.
Solar heating. Total direct irradiance within the Earths atmosphere.
1975
1975
1975
ESDU
ESDU
ESDU
0
0
0
1677
1678
1679
1680
1681
1682
1683
1684
1685
1686
1687
1688
1689
1690
1691
1692
1693
1694
1695
1696
1697
1698
1699
1700
1701
1702
1703
1704
1705
1706
1707
75018
Estimation of cruise range: propeller-driven aircraft.
66024 A
Approximate data on the viscosity of some common liquids.
75004
Wave drag of wings at zero lift in inviscid airflow.
75028
Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds.
AERO 00.01.09 A simple model of a thermally perfect, calorically imperfect diatomic gas. Comparison with real gases.
A
75027
Critical pressure coefficient and component of local Mach number normal to the surface isobar for a swept wing.
74008 A
Estimation of critical Mach number for an aerofoil from its low-speed pressure distribution.
73015 A
Estimation of the local buckling stress under biaxial compression of an isotropic skin with fibre reinforced integral
unflanged stiffeners.
FAT A.00.01 A The effect of mean stress on fatigue strength (plain test piece).
AERO
Conditions for shock wave detachment and for subsonic flow behind nose shock waves on cones at zero incidence and on
S.00.03.16 B
wedges.
75022
Design against fatigue. Basic design calculations.
AERO
Effect of cut-out on lift-curve slope.
W.01.01.04 A
74041
Example of the use of Data Items on range performance.
74042
Non-dimensional methods for the measurement of level-flight performance of turbine-engined helicopters.
TM 58
Comparison of surface pressure fluctuations in a turbulent boundary layer as measured on various flight vehicles
AERO
Limit of surface waviness for laminar flow over wings.
W.02.04.11 B
74043
Flexibilities of and stresses in unrestrained pressurised thin pipe bends subjected to in-plane bending.
STRUCT
Flexible circular frames supporting a shell. Displacements due to concentrated loads and couples.
03.06.15 A
74010 A
Low-speed drag coefficient increment at zero lift due to full-span split flaps.
74027
The effect of surface roughness on the fatigue limit of steels (at zero mean stress).
73011 A
Damping in acoustically excited structures.
67034 A
Effect of inclined nut seatings on the fatigue strength of steel screw threads.
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a skin with Z-section stringers.
02.01.35 B
STRUCT
Sandwich panels with corrugated core and equal face plates. Transverse shear stiffness.
07.03.01 A
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a corrugated sandwich panel.
02.01.37 B
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a skin with top hat section stringers.
02.01.36 B
74013
A method for estimating drag-rise Mach number at zero incidence of smooth or bumpy non-ducted axisymmetric bodies
without or with fins.
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a skin with integral unflanged stiffeners.
02.01.34 B
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a skin with integral unflanged stiffeners.
02.01.34
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a skin with Z-section stringers.
02.01.35
STRUCT
Estimation of the initial buckling stress under uniaxial compression of a skin with top hat section stringers.
02.01.36
1975
1975
1975
1975
1975
ESDU
ESDU
ESDU
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0
0
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0
1975
1975
1975
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1975
1975
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0
1975
1974
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0
1974
1974
1974
1974
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0
1974
1974
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0
1974
1974
1974
1974
1974
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0
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1974
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0
1974
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1974
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0
1974
ESDU
0
1974
ESDU
0
1974
ESDU
0
1974
ESDU
0
1974
ESDU
0
1708
1712
STRUCT
02.01.37
STRUCT
02.01.28
STRUCT
02.04.02
STRUCT
02.04.05
67011 A
1713
68019 B
1714
1715
70002
72025
1716
1717
69012 B
STRUCT
02.01.28 B
AERO 00.03.26 Wall and average gas temperatures for subsonic turbulent flow with heat transfer in ducts of constant circular cross section. 1973
A
STRUCT
Flexible circular frames supporting a shell. The effect of adjacent frames and the longitudinal flexibility of the shell.
1973
03.06.17 A
70002 A
Buckling stress ratios for flat plates under shear and non-uniform compression.
1973
70022 A
Non-dimensional graphical method for the analysis of measurements of steady level speed, range and endurance: aircraft
1973
with turbo-jet and turbo-fan engines.
FAT A.05.02 B Estimation of endurance of pin joints.
1973
71020 A
Aerofoils having a specified form of upper-surface pressure distribution: details and comments on design.
1973
STRUCT
Average and edge stresses for flat plates under shear and compression.
1973
02.04.02 A
AERO
Stability derivative (L sub v) sub gamma. Contribution of full-span dihedral to rolling moment due to sideslip.
1973
A.06.01.03 B
73031
Convective heat transfer during crossflow of fluids over plain tube banks.
1973
AERO
Drag of a smooth flat plate at zero incidence.
1973
W.02.04.01 B
STRUCT
Initial buckling of flat plates under compression, bending and shear.
1973
02.04.05 A
AERO
Normal force on flaps and controls.
1973
F.05.01.01 A
73016
The mean skin friction coefficient for a rough flat plate with a turbulent two-dimensional boundary layer in compressible
1973
adiabatic flow, with application to wedges, cylinders and cones.
69010 B
Heat transfer by forced convection between a two-dimensional laminar boundary layer and a smooth flat plate, with
1973
application to wedges, cylinders and cones.
FAT A.00.02 A The effect of mean stress on fatigue strength (test piece with stress concentration).
1973
AERO
Limit of grain size for laminar flow over wings or bodies.
1973
W.02.04.09 B
73012
Method for predicting the pressure distribution on swept wings with subsonic attached flow.
1973
70015 B
Fluid forces and moments on flat plates.
1972
1709
1710
1711
1718
1719
1720
1721
1722
1723
1724
1725
1726
1727
1728
1729
1730
1731
1732
1733
1734
1735
Estimation of the initial buckling stress under uniaxial compression of a corrugated sandwich panel.
1974
ESDU
0
Information on the use of Item No. 73007.
1973
ESDU
0
Average and edge stresses for flat plates under shear and compression.
1973
ESDU
0
Initial buckling of flat plates under compression, bending and shear.
1973
ESDU
0
Profile drag at the drag-rise condition of aerofoils having a specified form of upper-surface pressure distribution at this
1973
condition.
The compressible two-dimensional laminar boundary layer, both with and without heat transfer, on a smooth flat plate, with 1973
application to wedges, cylinders, and cones.
Buckling stress ratios for flat plates under shear and non-uniform compression.
1973
Second-order method for estimating the subcritical pressure distribution on a two-dimensional aerofoil in compressible
1973
inviscid flow.
Effects of kinetic heating on equilibrium temperature of flight vehicles.
1973
Information on the use of Item No. 73007.
1973
ESDU
0
ESDU
0
ESDU
ESDU
0
0
ESDU
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0
ESDU
0
ESDU
0
ESDU
ESDU
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0
ESDU
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ESDU
0
0
0
ESDU
0
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0
ESDU
0
ESDU
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ESDU
0
ESDU
ESDU
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ESDU
ESDU
0
0
1736
1737
1738
1739
1740
1741
1742
1743
1744
1745
1746
1747
1748
1749
1750
1751
1752
1753
1754
1755
1756
1757
1758
1759
1760
1761
1762
1763
1764
1765
1766
1767
1768
1769
1770
1771
1772
1773
72018
Atmospheric data for performance calculations. Addendum: height in feet, data in SI units.
AERO 00.01.07 Approximate transport properties of high-temperature air in dissociation equilibrium.
A
72002
The estimation of near-field sound pressure levels due to jet noise.
72013
Principal stresses and strains in a two-dimensional stress field.
PD1
The evaluation of Chebyshev series used for the representation of vapour pressures.
72014
Determination of the principal stresses and strains in a plane stress field from strain gauge data.
TM 4
Correlations for some aerodynamic characteristics of aerofoils in incompressible inviscid flow
72006
Normal melting points, boiling points and critical points of monobasic alkanoic acids.
67028 A
Estimation of the r.m.s. stress in skin panels subjected to random acoustic loading.
68040 B
Design of parallel axis straight spur and helical gears - choice of materials and preliminary estimate of major dimensions.
67029 A
The effect of edge reinforcement on the stresses in skin panels under uniform pressure.
72008
Frictional and retarding forces on aircraft tyres. Part III: planing.
72013
Principal stresses and strains in a two-dimensional stress field.
72014
Determination of the principal stresses and strains in a plane stress field from strain gauge data.
72027
Adaptation of drag-rise charts in T.D. Memor. 71019 to the mid-semi-span portion of swept and tapered planforms.
71018
Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow.
71001
Normal melting points, boiling points and critical points of n-alkyl esters of monobasic n-alkanoic acids.
71011
Stresses due to interference-fit pins and bushes in plates, strips or lugs
71017
Aero-normalised stability derivatives: effect of wing on yawing moment due to yawing.
71007
Low-speed normal force and pitching moment of slender wings in ground effect.
71021
Normal melting points, boiling points and critical points of branched chain esters of monobasic alkanoic acids.
71006
Low-speed longitudinal aerodynamic characteristics of slender wings.
71003
A guide to the viscosity of liquid petroleum products.
71012
Fluid forces on non-streamline bodies - background notes and description of the flow phenomena.
AERO
One-dimensional isentropic flow of a thermally perfect, calorically imperfect diatomic gas.
S.00.01.10 A
70018
General principles of design in relation to fatigue.
69025
Solution of ordinary linear differential equations by the Laplace transform method.
70021
Graphical method for the analysis of measured performance data using drag determination: aircraft with turbo-jet and
turbo-fan engines.
70020
Non-dimensional approach to engine thrust and airframe drag for the analysis of measured performance data: aircraft with
turbo-jet and turbo-fan engines.
70008
Inviscid supersonic flow past cones at zero incidence: (i) shock angle.
70009
Inviscid supersonic flow past cones at zero incidence: (iii) flow deflection in the conical flow field.
69004 A
Convective heat transfer during forced crossflow of fluids over a circular cylinder including free convection effects.
69003 A
The buckling of flat plates under non-uniform compression. Symmetric distributions due to initial or thermal stress.
70010
Inviscid supersonic flow past cones at zero incidence: (iv) Mach number in the conical flow field.
69003
The buckling of flat plates under non-uniform compression. Symmetric distributions due to initial or thermal stress.
67020
Fatigue strength of steel screw threads with large root radii under axial loading.
69017
The deflections and slopes of shafts or beams of constant or stepped section.
69020
Elastic stress concentration factors. Geometric discontinuties in flat bars or strips of isotropic material.
1972
1972
ESDU
ESDU
0
0
1972
1972
1972
1972
1972
1972
1972
1972
1972
1972
1972
1972
1972
1971
1971
1971
1971
1971
1971
1971
1971
1971
1971
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
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0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
1970
1970
1970
ESDU
ESDU
ESDU
0
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1970
ESDU
0
1970
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1969
1969
1969
ESDU
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ESDU
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0
0
0
0
0
0
0
0
0
1774
1775
1776
1777
69013
STRUCT
02.00.00 A
69011
A method for estimating the pressure distribution on the surface of a two-dimensional aerofoil in a sonic stream.
Criteria of yielding and failure.
1969
1969
ESDU
ESDU
0
0
Heat transfer by forced convection between a two-dimensional turbulent boundary layer and a smooth flat plate, with
application to wedges, cylinders and cones.
Criteria of yielding and failure.
1969
ESDU
0
1969
ESDU
0
Fatigue strength of steel screw threads with large root radii under axial loading.
Elastic stresses and deflections for long rectangular plates with small initial curvature under uniformly distributed normal
pressure on the concave face.
The deflections and slopes of shafts or beams of constant or stepped section.
Heat balance for flight vehicles.
The cumulative damage of aluminium alloy specimens under variable amplitude fatigue loading.
Curves for use in the determination of gross thrust and mass flow in flight. (Air breathing ducted-flow engines with
convergent nozzles.)
A method for estimating the pressure distribution between the crest and the trailing edge on the surface of an aerofoil
section in a sonic stream.
Experimental determination of the shear and flexural stiffnesses of a sandwich panel.
Geometric stress concentrations. Two equal unreinforced circular holes in infinite flat plates.
Introductory memorandum on the viscosity of liquids and the classification of lubricating oils.
Shafts with interference-fit collars. Part IV: fatigue strength of plain shafts.
Straight pipes under internal pressure. Effect of initial non-circularity on maximum stress.
Straight pipes under internal pressure. Effect of bore eccentricity on maximum stress.
Guide to the design of tanks for forced-circulation oil-lubrication systems.
Fatigue strength of large steel screw threads under axial loading.
Geometric stress concentrations. Two equal unreinforced circular holes in infinite flat plates.
Elastic stresses in single lap joints under tension or compression
Elastic stresses in single lap joints under tension or compression
The design of crossed flexure-pivots.
Elastic stresses in the torispherical head of a pressure vessel of uniform thickness.
Graphical method for estimating the spanwise distribution of aerodynamic centre on wings in subsonic flow.
1969
1969
ESDU
ESDU
0
0
1969
1969
1969
1969
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1969
ESDU
0
1969
1969
1968
1968
1968
1968
1968
1968
1967
1967
1967
1967
1967
1967
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
0
0
0
0
0
0
0
1967
1967
1966
1966
1966
1965
1965
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
ESDU
0
0
0
0
0
0
0
1965
ESDU
0
1965
1965
ESDU
ESDU
0
0
1778
1779
STRUCT
02.00.00
67020 A
69019
1780
1781
1782
1783
69017
69009
69024
69008
1784
TD MEMO
6511 A
66025 A
67023 A
68036
68005
68048
68047
68039
68045
67023
67008
67008
67021
67017
TD MEMO
6309 A
67022
Modulus of rigidity of sandwich panels with hexagonal cell cores.
67041
Drag of fighter-type canopies at subcritical Mach numbers.
66010
Elastic stresses in a long circular cylindrical shell with a flat head closure under uniform pressure.
66034
The low-speed stalling characteristics of aerodynamically smooth aerofoils.
66008
Design for minimum weight. Struts of uniform section. Minimum weights for various sections.
FAT E.07.03
The effect of mean stress on the endurance of aluminium alloys.
AERO 00.03.31 Solutions to the Prandtl-Meyer expansion relations for a range of specific heat ratios: pressure coefficient and maximum
flow deflection angle.
AERO
Base pressure on aerofoil sections with a blunt trailing edge in supersonic flow.
W.S.02.03.07
65002
Elastic stresses and deflections for flat circular plates with D/t greater than or equal to 4 under uniform pressure.
65002
Elastic stresses and deflections for flat circular plates with D/t greater than or equal to 4 under uniform pressure.
1785
1786
1787
1788
1789
1790
1791
1792
1793
1794
1795
1796
1797
1798
1799
1800
1801
1802
1803
1804
1805
1806
1807
1808
1809
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1811
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1818
1819
1820
1821
1822
1823
1824
1825
1826
1827
1828
1829
1830
1831
1832
1833
65003
FAT E.07.02
65008
STRUCT
02.01.50
STRUCT
02.01.50
STRUCT
02.01.48
STRUCT
02.01.48
STRUCT
03.06.00
STRUCT
03.06.16
STRUCT
01.01.23
STRUCT
01.01.23
STRUCT
01.01.19
STRUCT
02.01.46
STRUCT
02.04.06
STRUCT
02.04.06
STRUCT
02.01.46
STRUCT
01.06.01
STRUCT
01.06.00
STRUCT
01.06.03
STRUCT
01.06.02
STRUCT
01.06.00
STRUCT
01.06.01
STRUCT
01.06.02
STRUCT
01.06.03
AERO
W.S.02.03.09
Elastic stresses and deflections for flat circular plates with D/t greater than or equal to 20 under uniform pressure.
Notes supplementary to E.07.01 on the fatigue strength of aluminium alloys.
Viscosity of liquid benzene.
Initial buckling of slightly curved plates under combined longitudinal and circumferential direct stress. (All edges simplysupported.)
Initial buckling of slightly curved plates under combined longitudinal and circumferential direct stress. (All edges simplysupported.)
Buckling stress coefficients for flat plates tapered in plan, under compression.
1965
1965
1965
1964
ESDU
ESDU
ESDU
ESDU
0
0
0
0
1964
ESDU
0
1963
ESDU
0
Buckling stress coefficients for flat plates tapered in plan, under compression.
1963
ESDU
0
Information on the use of data sheets 03.06.
1962
ESDU
0
Flexible circular frames supporting a shell. Shear flow from shell to frame due to concentrated loads and couples.
1962
ESDU
0
The buckling of a composite strut.
1962
ESDU
0
The buckling of a composite strut.
1962
ESDU
0
Local buckling and crippling of rectangular tube section struts.
1960
ESDU
0
Buckling stress coefficients for flat parallelogram plates under uniform compression. (All edges fixed against rotation.)
1957
ESDU
0
Initial buckling of flat isosceles triangular plates under combined compression and shear.
1957
ESDU
0
Initial buckling of flat isosceles triangular plates under combined compression and shear.
1957
ESDU
0
Buckling stress coefficients for flat parallelogram plates under uniform compression. (All edges fixed against rotation.)
1957
ESDU
0
Form factors for circular sections under combined bending and axial load.
1956
ESDU
0
Information on the use of data sheets 01.06.
1956
ESDU
0
Form factors for angle, tee and channel sections under combined bending and axial load.
1956
ESDU
0
Form factors for flanged sections under combined bending and axial load.
1956
ESDU
0
Information on the use of data sheets 01.06.
1956
ESDU
0
Form factors for circular sections under combined bending and axial load.
1956
ESDU
0
Form factors for flanged sections under combined bending and axial load.
1956
ESDU
0
Form factors for angle, tee and channel sections under combined bending and axial load.
1956
ESDU
0
Transonic drag rise of rectangular symmetrical section wings at zero lift. NACA 65 series sections.
1955
ESDU
0
1834
1835
1836
1837
1838
1839
1840
1841
1842
1843
STRUCT
Flexible circular frames supported by a shell. Shear forces in a frame due to concentrated couples.
03.06.12
STRUCT
Flexible circular frames supported by a shell. Shear forces in a frame due to tangential loads.
03.06.13
STRUCT
Flexible circular frames supported by a shell. Shear forces in a frame due to concentrated radial loads.
03.06.14
STRUCT
Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated tangential loads.
03.06.10
STRUCT
Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated radial loads.
03.06.11
STRUCT
Flexible circular frames supported by a shell. Moments in a frame due to concentrated tangential loads.
03.06.07
STRUCT
Flexible circular frames supported by a shell. Moments in a frame due to concentrated radial loads.
03.06.08
STRUCT
Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated couples.
03.06.09
STRUCT
Flexible circular frames supported by a shell. Moments in a frame due to concentrated couples.
03.06.06
AERO 00.03.05 Isentropic expansion of air from rest.
Hercules Ebooks Institute
www.herculesebooks.com info@herculesebooks.com +989141908737
1952
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1952
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1952
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1952
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1952
ESDU
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1952
ESDU
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1952
ESDU
0
1952
ESDU
0
1952
ESDU
0
1948
ESDU
0