Richard P. Ray, Ph.D., P.E.
Civil and Environmental Engineering
University of South Carolina
USC
Thanks To:
Prof. Richard D. Woods, Notre Dame Univ.
Prof. F.E. Richart, Jr.
USC
Fundamentals
Modeling
Properties
Performance
USC
Z
Y
θ
φ
X
ψ
Fundamentals -Modeling-Properties-Performance USC
How Does It Fail?
Static Settlement
Dynamic Motion Too Large (0.02 mm is large)
Settlements Caused By Dynamic Motion
Liquefaction
What Are Maximum Values of Failure?
(Acceleration, Velocity, Displacement)
Fundamentals -Modeling-Properties-Design-Performance USC
Fundamentals
Massarch (2004) "Mitigation of Traffic-Induced Ground Vibrations"
-Modeling-Properties-Performance USC
Fundamentals -Modeling-Properties-Performance USC
What Are Relations Between Loads And
Failure Quantities
Loading -Machine (Periodic), Impluse, Natural
Relations Between Load, Structure, Foundation,
Soil, Neighboring Structures
Generate Model: Deterministic or Probabilistic
Fundamentals -Modeling-Properties-Performance USC
How Do We Measure What Is Necessary?
Full Scale Tests
Prototype Tests
Small Scale Tests (Centrifuge)
Laboratory Tests (Specific Parameters)
Numerical Simulation
Fundamentals -Modeling-Properties-Performance USC
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What Factor of Safety Do We Use?
Does FOS Have Meaning
What Happens After There Is Failure
Loss of Life
Loss of Property
Loss of Production
Purpose of Project, Design Life, Value
Fundamentals -Modeling-Properties-Performance USC
r -2 r -2 r -0.5
+
Rayleigh wave
Vertical component
Horizontal component
+
r -1
+
Shear wave
+
-
Relative amplitude
Shear window r -1
+
Fundamentals -Modeling-Properties-Performance
+ r
Wave Type Percentage of
Total Energy
Rayleigh
Shear
Compression
67
26
7
USC
Lumped Parameter (m,c,k) Block System
Parameters Constant, Layer, Special
Impedance Functions
Function of Frequency (ω), Layers
Boundary Elements (BEM)
Infinite Boundary, Interactions, Layers
Finite Element/Hybrid (FEM, FEM-BEM)
Complex Geometry, Non-linear Soil
FundamentalsModeling -Properties-Performance USC
P
P o sin(
t ) r m m c
G
ν ρ k m z c kz
P
0 sin(
t )
FundamentalsModeling -Properties-Performance USC
SDOF
Mag
A dynamic
A static
1
1
n
2
2
2 D
n
2
FundamentalsModeling -Properties-Performance USC
Z m z
z c z z k z z
P
0 sin(
t )
C z
I
ψ ψ
K z m
K x
n
X k m
C x
K
ψ
D
c c cr
C
ψ
/2 C
ψ
/2
FundamentalsModeling -Properties-Performance c cr
2 k m
USC
Lumped Parameter Values
Mode Vertical Horizontal Rocking Torsion
Stiffness k
Mass Ratio m
ˆ
Damping
Ratio, D
Fictitious
Mass
4 Gr
1
m ( 1
4
r
3
)
0 .
425
ˆ 1 / 2
0 .
27 m
8 Gr m
2
( 2
8
r
3
)
0 .
288
ˆ 1 / 2
0 .
095 m
8 Gr
3
3 ( 1
3 I
( 1
)
8
r
5
)
( 1
0 .
15
ˆ
)
ˆ 1 / 2
0 .
24 I x
16 Gr
3
3
I
r 5
0 .
50
1
2
0 .
24 I z
D=c/c cr
G=Shear Modulus ν=Poisson's Ratio r=Radius
ρ=Mass Density I
ψ
,I
θ
=Mass Moment of Inertia
USC FundamentalsModeling -Properties-Performance
FundamentalsModeling -Properties-Performance USC
VERTICAL COMPRESSOR
Unbalanced Forces
•Vertical Primanry = 7720 lb
•Vertical Secondary = 1886 lb
•Horzontal Primary = 104 lb
•Horizontal Secondary = 0 lb
Operating Speed = 450 rpm
Wt Machine + Motor = 10 900 lb
DESIGN CRITERION:
Smooth Operation At Speed
Velocity <0.10 in/sec
Displacement < 0.002 in
Soil Properties
Shear Wave Velocity V s
= 680 ft/sec
Shear Modulus, G = 11 000 psi
Density, γ = 110 lb/ft 3
Poisson's Ratio, ν = 0.33
USC FundamentalsModeling -Properties-Performance
A zs
Q
0 k z
0 .
002 " r
72 .
8 "
6 .
07 '
( 1
) Q
0
4 Gr
0 .
667 ( 7720
1885 )
4
11 000
r
Try a 15 x 8 x 3 foundation block, Area = 120 ft 2 and r = 6.18 ft
Weight = 54,000 lb Total Weight = 54 000 + 10 900 = 64 900
( 1
) W
4 r
3 g
g
0 .
67
4
110
64 900
6 .
18
3
0 .
42
D
0 .
425
0 .
66 M z
1 .
0
1
2 D
A z dynamic
A z static
0 .
002 "
FundamentalsModeling -Properties-Performance USC
34'
18'
Design Example - Table Top
W=550 000 lb
Q
0
=400 lb
I
ψ
=2.88 x 10 6 ft-lb-sec 2
18'
11'
Soil Properties
Shear Wave Velocity V s
= 770 ft/sec
Shear Modulus, G = 14 000 psi
Density, γ = 110 lb/ft 3
Poisson's Ratio, ν = 0.33
ψ
DESIGN CRITERION
0.20 in/sec Horizontal Motion at
Machine Centerline
Ax = 0.0015 in. from combined rocking and sliding
Speed = 160 rpm
Slower speeds, Ax can be larger
USC FundamentalsModeling -Properties-Performance
Horizontal Translation Only
Equivanlen t r
D
0 .
288
ˆ 1 / 2
0 .
465
4 cd
4
18
34
Mag x
1 .
0
13 .
96 ft
A x static
Q
0 k x
Q
0
8
2
2
8
Gr m
r
3
0 .
38
3 .
0
10
5 in
Rocking About Point "O"
Equivalent r
4
16 cd
3
3
4
16
17
9
3
3
12 .
0 ft
120 rpm
12 .
5 rad / sec k
D
2
8 Gr
8
( 14 000
144 )
12 .
04
2
0 .
33
2 .
90
10
8 lb / ft
n
k
I
2 .
90
10
8
2 .
88
10
6
10 rad / sec
3 ( 1
)
8
I
r
5
3 ( 0 .
67 )
8
2 .
88
10
6
110
32 .
2
( 12 .
04 )
5
0 .
83
( 1
0 .
15
)
0 .
09
Mag
5 .
6 Static Moment
M o
400
18
7200 ft
lbs .
FundamentalsModeling -Properties-Performance USC
Static Angular Deflection
s
M o k
7200
3 ( 0 .
67 )
2 .
9
10
8
0 .
50 rad
10
6
Horizontal
At
Motion
Resonance
A xs
s
5 .
6 ( 1 .
0
10
4
)
h
0 .
50
( 18
12 )
10
6
5 .
6
10
4 in .
1 .
0
10
4 in
6
5
4
3
2
1
0
0
Damping = 9%
0.5
1
OmegaRatio
1.5
FundamentalsModeling -Properties-Performance
2 2.5
USC
Based on Elasto-Dynamic Solutions
Compute Frequency-Dependent Impedance
Values (Complex-Valued)
Solved By Boundary Integral Methods
Require Uniform, Single Layer or Special Soil
Property Distribution
Solved For Many Foundation Types
USC FundamentalsModeling -Properties-Performance
P
P o e i
t
P o
cos(
t )
i sin(
t )
S z
S z
R z
A z
K
i
C
K
STATIC
k (
)
i
C
2 K
D
SOIL
Radiation Damping
FundamentalsModeling -Properties-Performance
Soil Damping
USC
Impedance Functions a
0
r
G
r
V s
ψ
Luco and Westmann (1970)
FundamentalsModeling -Properties-Performance USC
FundamentalsModeling -Properties-Performance USC
ψ
FundamentalsModeling -Properties-Performance USC
Boundary Element
Stehmeyer and Rizos, 2006
FundamentalsModeling -Properties-Performance USC
B-Spline Impulse Response Approach
FundamentalsModeling -Properties-Performance USC
e i
t
e i
t
2
then
Finite/Hybrid
Model
G *
G 1
2
2
2 i
1
2
FundamentalsModeling -Properties-Performance USC
Dynamic p-y Curves
FundamentalsModeling
Tahghighi and Tonagi 2007
-Properties-Performance USC
Shear Modulus, G and Damping Ratio, D
Soil Type
Confining Stress
Void Ratio
Strain Level
Field: Cross-Hole, Down-Hole, Surface
Analysis of Seismic Waves SASW
Laboratory: Resonant Column, Torsional
Simple Shear, Bender Elements
Fundamentals-ModelingProperties -Performance USC
Oscilloscope
ASTM D 4428
Pump
t
Shear Wave Velocity:
V s
=
x/
t
Test
Depth
Downhole
Hammer
(Source) packer
Note: Verticality of casing must be established by slope inclinometers to correct distances
x with depth.
Slope
Inclinometer
PVC-cased
Borehole
x
Velocity
Transducer
(Geophone
Receiver)
PVC-cased
Borehole
Slope
Inclinometer
USC
Resonant Column Test
G, D for Different γ
Fundamentals-ModelingProperties -Performance USC
Schematic Stress-Strain
Fundamentals-ModelingProperties -Performance USC
Hollow Cylinder RC-TOSS
Fundamentals-ModelingProperties -Performance USC
TOSS Test Results
Fundamentals-ModelingProperties -Performance USC
Steam Turbine-Generator
(Moreschi and Farzam, 2003)
Fundamentals-Modeling-PropertiesPerformance USC
Machine Foundation Design Criteria
Deflection criteria: maintain turbine-generator alignment during machine operating conditions
Dynamic criteria: ensure that no resonance condition is encountered during machine operating conditions
Strength criteria: reinforced concrete design
Fundamentals-Modeling-PropertiesPerformance USC
STG Pedestal Structure
Fundamentals-Modeling-PropertiesPerformance USC
Vibration Properties Evaluation
Identification of the foundation natural frequencies for the dominant modes
F requency exclusion zones for the natural frequencies of the foundation system and individual structural members (±20%)
Eigenvalue analysis: natural frequencies, mode shapes, and mass participation factors
USC Fundamentals-Modeling-PropertiesPerformance
Finite Element Model
Structure and Base
Fundamentals-Modeling-PropertiesPerformance USC
Low Frequency Modes
1 st mode
6.5 Hz
95 % m.p.f.
2 nd mode
7.2 Hz
76 % m.p.f
Fundamentals-Modeling-PropertiesPerformance USC
High Frequency Modes
28 th mode
46.3 Hz
0.3% m.p.f
Excitation frequency: 50-60 Hz
42 nd mode
64.6 Hz
0.03% m.p.f
USC Fundamentals-Modeling-PropertiesPerformance
Local Vibration Modes
Identification of natural frequencies for individual structural members
Quantification of changes on vibration properties due to foundation modifications
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-PropertiesPerformance USC
Optics Lab mass/Instrument weight = 228 tons
Wind mean force = 75 N, RMS = 89 N
Ground base excitation PSD = 0.004 g 2 /hz
Concrete Pier
High Strength Concrete (E=3.1
10 10 N/m 2 ,
=0.15)
Soil Stiffness, k
Four different values using Arya & O’Neil’s formula based on the site test data (Shear modulus:30~75ksi, Poisson’s ratio:0.35~0.45)
USC Fundamentals-Modeling-PropertiesPerformance
Frequency vs Soil Stiffness
Stiffness units = SI, frequency mode (hz)
MODE
1
2
3
4
5
6
Stiffness
Kx
Ky
Kz
Krx
Kry
Krz min m in+33.3% m in+66.6% max
1.19E+10 1.83E+10 2.48E+10 3.12E+10
1.19E+10 1.83E+10 2.48E+10 3.12E+10
1.48E+10 2.45E+10 3.41E+10 4.38E+10
1.34E+12 2.21E+12 3.09E+12 3.96E+12
1.34E+12 2.21E+12 3.09E+12 3.96E+12
1.74E+12 2.61E+12 3.49E+12 4.36E+12
6.3
7.0
7.4
7.5
6.4
9.4
7.1
9.7
7.5
9.9
7.7
10
9.4
10.4
11.2
10.3
11.9
13.0
11.1
12.6
13.6
11.8
13.3
13.7
• Soil property range: Shear modulus (30~75ksi), Poisson’s ratio (0.35~0.45)
• Pier Footing: Diameter (23.3m)
• “min” for shear modulus of 30 ksi; “max” for 75 ksi
Fundamentals-Modeling-PropertiesPerformance USC
Summary and Conclusions (Cho, 2005)
1.
High fidelity FE models were created
2.
Relative mirror motions from zenith to horizon pointing: about 400 m m in translation and 60 m rad in rotation.
3.
Natural frequency changes by 2 hz as height changes by 10m.
4.
Wind buffeting effects caused by dynamic portion (fluctuation) of wind
5.
Modal responses sensitive to stiffness of bearings and drive disks
6.
Soil characteristics were the dominant influences in modal behavior of the telescopes .
7.
Fundamental Frequency (for a lowest soil stiffness):
OSS=20.5hz; OSS+base=9.9hz; SS+base+Coude+soil=6.3hz
8.
A seismic analysis was made with a sample PSD
9.
ATST structure assembly is adequately designed:
1.
Capable of supporting the OSS
2.
3.
Dynamically stiff enough to hold the optics stable
Not significantly vulnerable to wind loadings
Fundamentals-Modeling-PropertiesPerformance USC
Free-Field Analytical Solutions u z u r u z
( r ,
, 0 )
i
2
L
0
V
3
R
V
( a
0
) H
0
2
r
C
R
u r
( r ,
, 0 )
i
2
M
3
0
V
R
V
( a
0
) H
1
2
r
C
R
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-PropertiesPerformance USC
Trench
Isolation
Karlstrom and Bostrom 2007
Fundamentals-Modeling-PropertiesPerformance USC
Fundamentals-Modeling-Properties-
Chehab and Nagger 2003
Performance USC
Celibi et al (in press)
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Questions?
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r -2 r -2 r -0.5
+
Rayleigh wave
Vertical component
Horizontal component
+
Shear window r -1
+
r -1
+
Shear wave
+
-
Relative amplitude
+ r
Wave Type Percentage of
Total Energy
Rayleigh
Shear
Compression
67
26
7
USC
Rayleigh, R
Surface
Shear,S
Secondary
Compression, P
Primary
USC
Machine Performance Chart
0.002
Performance Zones
A=No Faults, New
B=Minor Faults ,
Good Condition
C = Faulty, Correct
In 10 Days To Save
$$
D = Failure Is Near,
Correct In 2 Days
E = Stop Now
450
USC