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Oxford Cambridge and RSA
Level 3 Cambridge Technical in Engineering
05822/05823/05824/05825/05873
C
Formula Booklet
3
0
6
-
Unit 1 Mathematics for engineering
Unit 2 Science for engineering
Unit 3 Principles of mechanical engineering
Unit 4 Principles of electrical and electronic engineering
Unit 23 Applied mathematics for engineering
This booklet contains formulae which learners studying the above units and taking associated
examination papers may need to access.
Other relevant formulae may be provided in some questions within examination papers. However, in
most cases suitable formulae will need to be selected and applied by the learner. Clean copies of this
booklet will be supplied alongside examination papers to be used for reference during examinations.
Formulae have been organised by topic rather than by unit as some may be suitable for use in more
than one unit or context.
Note for teachers
This booklet does not replace the taught content in the unit specifications or contain an exhaustive
list of required formulae. You should ensure all unit content is taught before learners take associated
examinations.
© OCR 2021 [L/506/7266, R/506/7267, Y/506/7268, D/506/7269, R/506/7270]
C306/XXXX/1
OCR is an exempt Charity
Version 6
1.
Trigonometry and Geometry
1.1 Geometry of 2D and 3D shapes
1.1.1. Circles and arcs
Circle: radius r
Area of a circle = πœ‹πœ‹π‘Ÿπ‘Ÿ 2
Circumference of a circle = 2πœ‹πœ‹πœ‹πœ‹
Co-ordinate equation of a circle: radius r, centre (a, b)
(π‘₯π‘₯ − π‘Žπ‘Ž)2 + (𝑦𝑦 − 𝑏𝑏)2 = π‘Ÿπ‘Ÿ 2
Arc and sector: radius r, angle θ
for θ expressed in radians
Arc length = πœƒπœƒπœƒπœƒ,
1
2
Area of sector = π‘Ÿπ‘Ÿ 2 πœƒπœƒ, for θ expressed in radians
Arc length =
πœƒπœƒ
πœ‹πœ‹πœ‹πœ‹,
180
Area of sector =
for θ expressed in degrees
πœƒπœƒ
πœ‹πœ‹πœ‹πœ‹ 2 ,
360
for θ expressed in degrees
Converting between radians and degrees
x radians =
180π‘₯π‘₯
πœ‹πœ‹
πœ‹πœ‹πœ‹πœ‹
degrees
x degrees = 180 radians
2
1.1.2 Triangles
1
2
Area = π‘π‘β„Ž or
1
𝑏𝑏𝑏𝑏 sin 𝐴𝐴
2
1.2 Volume and Surface area of 3D shapes
Cuboid
Surface area = 2𝑙𝑙𝑙𝑙 + 2π‘€π‘€β„Ž + 2β„Žπ‘™π‘™
= 2(𝑙𝑙𝑙𝑙 + π‘€π‘€β„Ž + β„Žπ‘™π‘™)
Volume = π‘™π‘™π‘™π‘™β„Ž
Sphere
Surface area = 4πœ‹πœ‹π‘Ÿπ‘Ÿ 2
4
3
Volume = πœ‹πœ‹π‘Ÿπ‘Ÿ 3
Cone
Surface area = πœ‹πœ‹π‘Ÿπ‘Ÿ 2 + πœ‹πœ‹πœ‹πœ‹πœ‹πœ‹
1
3
Volume = πœ‹πœ‹π‘Ÿπ‘Ÿ 2 β„Ž
3
Cylinder
Surface area = 2πœ‹πœ‹π‘Ÿπ‘Ÿ 2 + 2πœ‹πœ‹πœ‹πœ‹β„Ž
Volume = πœ‹πœ‹π‘Ÿπ‘Ÿ 2 β„Ž
Rectangular Pyramid
Volume =
π‘™π‘™π‘™π‘™β„Ž
3
Prism
Volume = area of shaded cross-section × l
Density
Density =
mass
volume
4
1.3 Centroids of planar shapes
1.4 Trigonometry
c
a
θ
b
π‘Žπ‘Ž
sin πœƒπœƒ =
𝑐𝑐
cos πœƒπœƒ =
tan πœƒπœƒ =
𝑏𝑏
𝑐𝑐
π‘Žπ‘Ž
𝑏𝑏
Pythagoras’ rule: 𝑐𝑐 2 = π‘Žπ‘Ž2 + 𝑏𝑏 2
C
b
a
A
Sine rule:
π‘Žπ‘Ž
sin 𝐴𝐴
Cosine rule:
B
c
=
𝑏𝑏
sin 𝐡𝐡
=
𝑐𝑐
sin 𝐢𝐢
π‘Žπ‘Ž2 = 𝑏𝑏 2 + 𝑐𝑐 2 − 2𝑏𝑏𝑏𝑏 cos 𝐴𝐴
5
1.4.1 Trigonometric identities
Basic trigonometric values
sin 60° =
√3
2
cos 60° =
1
2
tan 60° = √3
sin 45° = cos 45° =
tan 45° = 1
sin 30° =
cos 30° =
tan 30° =
Trigonometric identities
1
√2
1
2
√3
2
1
√3
sin 𝐴𝐴 = cos(90° − 𝐴𝐴) for angle A in degrees
cos 𝐴𝐴 = sin(90° − 𝐴𝐴) for angle A in degrees
πœ‹πœ‹
sin 𝐴𝐴 = cos �𝐴𝐴 − οΏ½
2
πœ‹πœ‹
cos 𝐴𝐴 = −sin �𝐴𝐴 − οΏ½
2
tan 𝐴𝐴 =
sin 𝐴𝐴
cos 𝐴𝐴
sin2 𝐴𝐴 + cos 2 𝐴𝐴 = 1
sin(−𝐴𝐴) = −sin 𝐴𝐴
cos(−𝐴𝐴) = cos 𝐴𝐴
sin(A ± B) = sinAcosB ± cos AsinB
cos(A ± B) = cos Acos B βˆ“ sinAsinB
sin 2𝐴𝐴 = 2 sin 𝐴𝐴 cos 𝐴𝐴
cos 2𝐴𝐴 = cos2 𝐴𝐴 − sin2 𝐴𝐴
6
2.
Calculus
2.1 Differentiation
f ( x)
df ( x )
dx
c
0
xn
nx n −1
sin ( ax )
a cos ( ax )
cos ( ax )
−a sin ( ax )
tan ( ax )
a sec 2 ( ax )
e ax
ae ax
ln ( ax )
1
x
ax
a x ln a
log a x
1
x ln a
2.1.1 Differentiation of the product of two functions
If 𝑦𝑦
= 𝑒𝑒 × π‘£π‘£
d𝑦𝑦
dπ‘₯π‘₯
= 𝑒𝑒
d𝑣𝑣
dπ‘₯π‘₯
+ 𝑣𝑣
d𝑒𝑒
dπ‘₯π‘₯
2.1.2 Differentiation of the quotient of two functions
𝑒𝑒
If 𝑦𝑦
=
If 𝑦𝑦
= 𝑒𝑒(𝑣𝑣)
𝑣𝑣
d𝑦𝑦
dπ‘₯π‘₯
=
d𝑒𝑒
d𝑣𝑣
𝑣𝑣 dπ‘₯π‘₯ − 𝑒𝑒dπ‘₯π‘₯
𝑣𝑣 2
2.1.3 Differentiation of a function of a function
d𝑦𝑦
dπ‘₯π‘₯
=
d𝑒𝑒 d𝑣𝑣
d𝑣𝑣 dπ‘₯π‘₯
7
2.2 Integration
2.2.1 Indefinite integrals
f(π‘₯π‘₯)
οΏ½ f(π‘₯π‘₯) dπ‘₯π‘₯ (+𝑐𝑐)
xn
x n +1
n +1
a
ax
for n ≠ −1
1
π‘₯π‘₯
ln x
eπ‘Žπ‘Žπ‘Žπ‘Ž
π‘Žπ‘Žπ‘Žπ‘Ž
e
π‘Žπ‘Ž
π‘Žπ‘Ž π‘₯π‘₯
ln π‘Žπ‘Ž
π‘Žπ‘Ž π‘₯π‘₯
− cos(π‘Žπ‘Žπ‘Žπ‘Ž)
π‘Žπ‘Ž
sin(π‘Žπ‘Žπ‘Žπ‘Ž)
sin(π‘Žπ‘Žπ‘Žπ‘Ž)
π‘Žπ‘Ž
cos(π‘Žπ‘Žπ‘Žπ‘Ž)
2.2.2 Definite integral
𝑏𝑏
𝑏𝑏
οΏ½ f (π‘₯π‘₯) dπ‘₯π‘₯ = [F(π‘₯π‘₯)]π‘Žπ‘Ž = F(𝑏𝑏) − F(π‘Žπ‘Ž)
π‘Žπ‘Ž
2.2.3 Integration by parts
οΏ½ 𝑒𝑒
d𝑣𝑣
d𝑒𝑒
dπ‘₯π‘₯ = 𝑒𝑒𝑒𝑒 − οΏ½ 𝑣𝑣 dπ‘₯π‘₯
dπ‘₯π‘₯
dπ‘₯π‘₯
8
3.
Algebraic formulae
3.1 Solution of quadratic equation
π‘Žπ‘Žπ‘₯π‘₯ 2 + 𝑏𝑏𝑏𝑏 + 𝑐𝑐 = 0, π‘Žπ‘Ž ≠ 0
⇒
π‘₯π‘₯ =
−𝑏𝑏 ± √𝑏𝑏 2 − 4π‘Žπ‘Žπ‘Žπ‘Ž
2π‘Žπ‘Ž
3.2 Exponentials/Logarithms
𝑦𝑦 = eπ‘Žπ‘Žπ‘Žπ‘Ž ⇒ ln 𝑦𝑦 = π‘Žπ‘Žπ‘Žπ‘Ž
4.
Measurement
Absolute error = indicated value – true value
Relative error =
absolute error
true value
Absolute correction = true value – indicated value
Relative correction =
absolute correction
true value
9
5. Statistics
For a sample, size N, π‘₯π‘₯1 , π‘₯π‘₯2 , π‘₯π‘₯3 , … , π‘₯π‘₯𝑁𝑁 ,
sample mean
π‘₯π‘₯Μ… =
standard deviation
π‘₯π‘₯1 +π‘₯π‘₯2 +π‘₯π‘₯3 +β‹―+π‘₯π‘₯𝑁𝑁
𝑁𝑁
S=
1
N
N
∑ (x − x)
i
i =1
2
=
1
N
N
∑x
i =1
2
i
− ( x )2
5.1 Probability
For events A and B, with probabilities of occurrence P(A) and P(B),
P(A or B) = P(A) + P(B) – P(A and B)
If A and B are mutually exclusive events,
P(A and B) = 0
P(A or B) = P(A) + P(B)
If A and B are independent events,
P(A and B) = P(A) x P(B)
10
6. Mechanical equations
6.1 Stress and strain equations
axial stress (σ) =
axial force
cross sectional area
axial strain (ξ) = change in length
original length
shear stress (τ) = shear force
shear area
Young’s modulus (E) = stress
strain
Working or allowable stress = ultimate stress
Factor of Safety (FOS)
6.2 Mechanisms
Mechanical advantage (MA) =
Velocity ratio (VR) =
velocity of input to a mechanism
•
Class one lever
•
Class two lever
•
Class three lever
𝐹𝐹0
𝐹𝐹I
=
input force (or torque)
velocity of output from a mechanism
6.2.1 Levers
MA =
output force (or torque)
π‘Žπ‘Ž
𝑏𝑏
𝑉𝑉𝑉𝑉 =
𝑉𝑉0
𝑉𝑉I
11
=
𝑏𝑏
π‘Žπ‘Ž
6.2.2 Gear systems
MA = Number of teeth on output gear
Number of teeth on input gear
VR = Number of teeth on input gear
Number of teeth on output gear
6.2.3 Belt and pulley systems
MA = Diameter of output pulley
Diameter of input pulley
VR = Diameter of input pulley
Diameter of output pulley
6.3 Dynamics
Newton’s equation force = mass x acceleration (𝐹𝐹 = π‘šπ‘šπ‘šπ‘š)
Gravitational potential energy (Wp) = mass x gravitational acceleration x height (mgh)
1
2
Kinetic energy (Wk) = ½ mass x velocity2 ( π‘šπ‘šπ‘£π‘£ 2 )
Work done = force x distance (Fs)
Instantaneous power = force x velocity (Fv)
π‘Šπ‘Š
𝑑𝑑
Average power = work done / time ( )
Friction Force ≤ coefficient of friction x normal contact force (𝐹𝐹 ≤ πœ‡πœ‡πœ‡πœ‡)
Momentum of a body = mass x velocity (mv)
Pressure
= force / area (
𝐹𝐹
𝐴𝐴
)
12
6.4 Kinematics
Constant acceleration formulae
a – acceleration
𝑣𝑣 2 = 𝑒𝑒2 + 2π‘Žπ‘Žπ‘Žπ‘Ž
s – distance
1
𝑠𝑠 = 𝑒𝑒𝑒𝑒 + π‘Žπ‘Žπ‘‘π‘‘ 2
2
t – time
u – initial velocity
𝑣𝑣 = 𝑒𝑒 + π‘Žπ‘Žπ‘Žπ‘Ž
v – final velocity
1
𝑠𝑠 = (𝑒𝑒 + 𝑣𝑣)𝑑𝑑
2
1
𝑠𝑠 = 𝑣𝑣𝑣𝑣 − π‘Žπ‘Žπ‘‘π‘‘ 2
2
6.5 Fluid mechanics
Pressure due to a column of liquid
= height of column × gravitational acceleration × density of liquid (hgρ)
Up-thrust force on a submerged body
= volume of submerged body × gravitational acceleration × density of liquid (Vgρ)
6.5.1 Energy equations
Non-flow energy equation
U1 + Q = U2 + W
so Q = (U2 – U1) + W
where Q = energy entering the system
W = energy leaving the system
U1 = initial energy in the system
U2 = final energy in the system.
Steady flow energy equation
Q = (W2 – W1) + W
where Q = heat energy supplied to the system
W1 = energy entering the system
W2 = energy leaving the system
W = work done by the system.
13
7. Thermal Physics
p – pressure
V – volume
C – constant
T – absolute temperature
n – number of moles of a gas
R – the gas constant
Boyle’s law
Charles’ law
𝑉𝑉
Pressure law
𝑝𝑝
Combined gas law
𝑝𝑝1 𝑉𝑉1
Ideal gas law
𝑝𝑝1 𝑉𝑉1 = 𝑝𝑝2 𝑉𝑉2
𝑝𝑝𝑝𝑝 = 𝐢𝐢
𝑇𝑇
𝑇𝑇
𝑉𝑉1
= 𝐢𝐢
= 𝐢𝐢
𝑇𝑇1
=
𝑇𝑇1
𝑝𝑝1
𝑝𝑝2 𝑉𝑉2
𝑇𝑇1
=
=
𝑉𝑉2
𝑇𝑇2
𝑝𝑝2
𝑇𝑇2
𝑇𝑇2
𝑝𝑝𝑝𝑝 = 𝑛𝑛𝑛𝑛𝑛𝑛
Characteristic gas law
𝑝𝑝𝑝𝑝 = π‘šπ‘šπ‘šπ‘šπ‘šπ‘š where m = mass of specific gas and
R = specific gas constant
Efficiency
πœ‚πœ‚ =
7.1 Heat formulae
work output
work input
Latent heat formula
Heat absorbed or emitted during a change of state, Q = mL
where Q = Energy, L = latent heat of transformation, m = mass
Sensible heat formula
Heat energy, Q = mcβˆ†T
where Q = Energy, m = mass, c = specific heat capacity of substance,
βˆ†T is change in temperature
14
8. Electrical equations
Q = charge
V = voltage
I = current
R = resistance
ρ = resistivity
P = power
E = electric field strength
(capacitors)
C = capacitance
L = inductance
t = time
l = length
τ = time constant
W = energy
A = cross sectional area
Φ = magnetic flux
N = number of turns
Ɵ = angle (in radians)
f = Frequency (in cycles per second)
ω = 2πf
XL, XC = inductive reactance, capacitive reactance
Z = impedance
Ø = phase angle
E = emf (motors)
Ia = armature current
If = field current
Il = load current
Ra = armature resistance
Rf = field resistance
n = speed (motors)
T = torque
Ι³ = efficiency
Charge and potential energy
Drift velocity (current)
Power
Resistance and Ohms law
Q = It
V = W/Q
W = Pt
I = nAve
P= VI
P = I 2R
P = V 2/R
Series resistance: R = R1 + R2 + R3 +…
Parallel resistance:
Resistivity
Electric field and capacitance
Inductance and self-inductance
RC circuits
AC waveforms
AC circuits – resistance and reactance
Series RL and RC circuits
Ohms law: R = V/I
ρ = RA/l
E = V/d
C = Q/V
W = ½QV
L =ΦN/ I
WL= ½LI 2
τ = RC
v = v e-t/RC
0
1
𝑅𝑅
=
1
𝑅𝑅1
V = IR
+
1
𝑅𝑅2
1
𝑅𝑅3
I = V/R
v = V sinƟ
i = I sinƟ
v = V sinωt
i = I sinωt
R = V/I
XL = V/I and XL = 2πfL
1
XC = V/I and XC =
2πfC
2
2
Z = √(R + XL ) and cosø = R/Z
Z = √(R2 + XC2) and cosø = R/Z
15
+
+…
Series RLC circuits
DC motor
DC generator
DC Series wound self-excited generator
DC Shunt wound self-excited generator
DC Series wound motor
DC Shunt wound motor - No-load
conditions:
DC Shunt wound motor - Full load
conditions:
Speed control of DC motors - Shunt motor
DC Machine efficiency
When XL > XC
Z = √[R2 + (XL – XC)2] and cosø = R/Z
When XC>XL
Z = √[R2 + (XC – XL)2] and cosø = R/Z
When XL= XC
Z=R
V = E + IaRa
V = E − IaRa
V = E − IaRt
Where Rt = Ra + Rf
V = E − IaRa
Where Ia = If + Il
If = V/Rf
Il = P/V
V = E + IaRt
Where Rt = Ra + Rf
E ∝ Φn
V = E1 + IaRa
Where Ia = Il − If
If = V/Rf
V = E2 + IaRa
Where Ia = Il − If
E1/E2 = n1/n2
T1/T2 = (Φ1Ia1)/(Φ2Ia2)
V = E + IaRa
n = (V − IaRa)/(kΦ)
Ι³ = output/input
Ι³ = 1 – (losses/input)
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16
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