Machine Design: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

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1Formulas and methods

Gears & gear trains

Meshing gears
n1·N1 = n2·N2
Torque
T2 = T1·(N2/N1)·η
Power
P = T·ω, ω = 2π·n/60
Compound train
total ratio = product of the stage ratios

Torsion of shafts

Shear stress
τ = T·r/J
Solid shaft
J = πd⁴/32
Hollow shaft
J = π(D⁴ − d⁴)/32
Angle of twist
φ = TL/(GJ)
Power
P = T·ω = 2πnT/60

Method

  1. Find the polar moment of area: J = πd⁴/32 for a solid shaft.
  2. Shear stress at the surface: τ = T·r/J, with r the outer radius.
  3. Angle of twist: φ = TL/(GJ) in radians.
  4. If power is given, find the torque first with P = T·ω, ω = 2πn/60.

Mohr’s circle & stress transformation

Centre
C = (σx + σy)/2
Radius
R = √(((σx − σy)/2)² + τxy²)
Principal stresses
σ1,2 = C ± R
Principal direction
tan 2θp = 2τxy/(σx − σy)
Inclined plane
σθ = C + (σx − σy)/2·cos 2θ + τxy·sin 2θ

Method

  1. Calculate the centre of Mohr’s circle: C = (σx + σy)/2.
  2. Calculate the radius: R = √(((σx − σy)/2)² + τxy²).
  3. The principal stresses are C ± R and the largest in-plane shear stress is R.
  4. Angles on the circle are double the angles on the element: tan 2θp = 2τxy/(σx − σy).

Axial stress & strain

Normal stress
σ = F/A
Strain
ε = ΔL/L
Hooke’s law
σ = E·ε
Elongation
ΔL = FL/(EA)
Thermal strain
εT = α·ΔT

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Mechanical vibrations

Natural frequency
ωn = √(k/m), fn = ωn/(2π)
From static deflection
ωn = √(g/δst)
Critical damping
cc = 2√(km) = 2mωn
Damping ratio
ζ = c/cc
Damped frequency
ωd = ωn√(1 − ζ²)
Logarithmic decrement
δ = (1/n)·ln(x0/xn), ζ = δ/√(4π² + δ²)
Springs in parallel
k = k1 + k2
Springs in series
1/k = 1/k1 + 1/k2

2Practice problems

1.Gears & gear trainsMedium
N1​ = ?N2​

Two parallel shafts are 240 mm apart. They must be connected by a pair of spur gears with a module of 4 mm and a speed reduction of 3 : 1. How many teeth N1 must the pinion have?

a = 240 mmm = 4 mmi = 3
N1 =
2.Gears & gear trainsHard
A = 20B = 30C = 24D = ?

In a compound gear train, gear A (20 teeth) on the input shaft turns at 2880 rpm and drives gear B (30 teeth). Gear C (24 teeth) is fixed to the same shaft as B and drives gear D on the output shaft. The output must turn at 640 rpm. How many teeth ND must gear D have?

nin = 2880 rpmA = 20B = 30C = 24nout = 640 rpm
ND =
3.Torsion of shaftsMedium
d = 20 mmT = 20 N·m400 mmφ = 1.12°

In a torsion test, a solid specimen of diameter 20 mm is twisted by a torque of 20 N·m. The two ends of a gauge length of 400 mm rotate 1.12° relative to each other (the material is still elastic). Find the shear modulus G of the material.

T = 20 N·md = 20 mmL = 400 mmφ = 1.12°
G = GPa
4.Torsion of shaftsHard
d = 60 mmTB​ = 200 N·mTC​ = 400 N·mABC0.5 m0.8 m

A solid aluminium shaft of diameter 60 mm is fixed at A. A torque of 200 N·m acts at B, 0.5 m from A, and a torque of 400 N·m in the same direction acts at the free end C, a further 0.8 m along. Find the maximum shear stress τmax in the shaft.

d = 60 mmTB = 200 N·mTC = 400 N·mAB = 0.5 mBC = 0.8 m
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = 10σy​ = −50τxy​ = −10MPa

A point in a loaded part has σₓ = 10 MPa, σᵧ = −50 MPa and τₓᵧ = −10 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = 10 MPaσy = −50 MPaτxy = −10 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 0σy​ = −20τxy​ = 40MPa

A point in a loaded part has σₓ = 0 MPa, σᵧ = −20 MPa and τₓᵧ = 40 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 50° counter-clockwise from the x-axis.

σx = 0 MPaσy = −20 MPaτxy = 40 MPaθ = 50°
σθ = MPa
7.Axial stress & strainMedium
P = ?12400 mm500 mmØ20Ø30δ = 0.2 mm

A bar is made of a steel segment (diameter 20 mm, length 400 mm, E = 200 GPa) joined end to end with a segment made of aluminium (diameter 30 mm, length 500 mm, E = 70 GPa). It is fixed at one end and pulled at the other. Find the axial load P that stretches it by 0.2 mm in total.

segment 1: steel, Ø20 mm, 400 mm, E = 200 GPasegment 2: aluminium, Ø30 mm, 500 mm, E = 70 GPaδ = 0.2 mm
P = kN
8.Axial stress & strainHard
30 kN12400 mm500 mmØ30Ø60σ2​ = ?

A steel segment (diameter 30 mm, length 400 mm, E = 200 GPa) and a segment made of aluminium (diameter 60 mm, length 500 mm, E = 70 GPa) are joined end to end and fixed between two rigid walls. An axial load of 30 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø30 mm, 400 mm, E = 200 GPasegment 2: aluminium, Ø60 mm, 500 mm, E = 70 GPaP = 30 kN
σ2 = MPa
9.Column bucklingMedium
PL = 1.5 md = 30 mmcross-section

A column of length L made of steel is fixed at the base and pinned at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 1.5 mE = 200 GPa (steel)d = 30 mm
Pcr = kN
10.Column bucklingHard
P = 90 kNL = 1.5 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and free at the top. It must carry 90 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 90 kNn = 2.5L = 1.5 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
k = 40 kN/mζ = 0.7m = 100 kg

A 100 kg mass on a spring with a stiffness of 40 kN/m has a viscous damper giving a damping ratio of 0.7. Find the damped natural frequency fd of its free vibration in Hz.

m = 100 kgk = 40 kN/mζ = 0.7
fd = Hz
12.Mechanical vibrationsHard
k1​ = 50k2​ = 10m = 40 kg

A 40 kg mass hangs from two springs connected end to end (in series): the upper spring has k₁ = 50 kN/m and the lower one k₂ = 10 kN/m. Ignore damping and the masses of the springs. Find the natural frequency fn of vertical vibration in Hz.

m = 40 kgk1 = 50 kN/mk2 = 10 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: N1 = 30

Gear geometry: the module m sets the tooth size. A gear with N teeth has a pitch diameter d = m·N, two meshing gears have the same module, and their centre distance is a = (d₁ + d₂)/2 = m·(N₁ + N₂)/2. The pitch-line speed is v = π·d·n/60, and the tangential tooth force follows from the torque: Ft = 2T/d.

Total number of teeth

N1 + N2 = 2a/m = 2·240/4 = 120

Split by the ratio

N1 = 120/(1 + 3) = 30

Answer

N1 = 30
2.Gears & gear trains

Answer: ND = 72

Gear trains: meshing gears have the same speed at the teeth, so n₁·N₁ = n₂·N₂: the gear with fewer teeth turns faster. Gears on one shaft turn at the same speed. Power is passed on (minus losses), so torque goes up when speed goes down: T₂ = T₁·(N₂/N₁)·η, and P = T·ω with ω = 2π·n/60.

Intermediate shaft speed

nB = nC = 2880·20/30 = 1920 rpm

Teeth on gear D

ND = C·nC/nout = 24·1920/640 = 72

Answer

ND = 72
3.Torsion of shafts

Answer: G = 26.05 GPa

Torsion of circular shafts: shear stress grows linearly from zero at the centre to τmax = T·r/J at the surface, with J = πd⁴/32 for a solid shaft and J = π(do⁴ − di⁴)/32 for a hollow one. The angle of twist is φ = TL/(GJ) in radians. Power and torque are linked by P = T·ω.

Polar moment and angle

J = π·20⁴/32 = 15708 mm⁴
φ = 1.12·π/180 = 0.01955 rad

Shear modulus

T = 20 N·m = 20000 N·mm
G = TL/(Jφ) = 20000·400/(15708·0.01955) = 26054 MPa
G = 26.05 GPa

Answer

G = 26.05 GPa

Compare: steel ≈ 80 GPa, brass ≈ 39 GPa, aluminium ≈ 26 GPa.

4.Torsion of shafts

Answer: τmax = 14.15 MPa

Torsion of circular shafts: shear stress grows linearly from zero at the centre to τmax = T·r/J at the surface, with J = πd⁴/32 for a solid shaft and J = π(do⁴ − di⁴)/32 for a hollow one. The angle of twist is φ = TL/(GJ) in radians. Power and torque are linked by P = T·ω.

Internal torques

Sense of TC taken as positive.

TBC = TC = 400 N·m
TAB = TC + TB = 400 + 200 = 600 N·m

Maximum shear stress

The segment with the largest internal torque has the largest stress (same diameter).

|T|max = 600 N·m
τmax = 16·600000/(π·60³) = 14.15 MPa

Answer

τmax = 14.15 MPa
5.Mohr’s circle & stress transformation

Answer: τmax = 31.62 MPa

Plane stress transformation: on a plane rotated by θ, σ = (σₓ + σᵧ)/2 + (σₓ − σᵧ)/2·cos 2θ + τₓᵧ·sin 2θ. Mohr’s circle shows all planes at once: its centre is at C = (σₓ + σᵧ)/2 and its radius is R = √(((σₓ − σᵧ)/2)² + τₓᵧ²). The principal stresses are C ± R, and the largest in-plane shear stress is R.

στxyCτmax​

Radius of Mohr’s circle

τmax = R = √(((10 − −50)/2)² + −10²) = 31.62 MPa

Answer

τmax = 31.62 MPa
6.Mohr’s circle & stress transformation

Answer: σθ = 27.66 MPa

Plane stress transformation: on a plane rotated by θ, σ = (σₓ + σᵧ)/2 + (σₓ − σᵧ)/2·cos 2θ + τₓᵧ·sin 2θ. Mohr’s circle shows all planes at once: its centre is at C = (σₓ + σᵧ)/2 and its radius is R = √(((σₓ − σᵧ)/2)² + τₓᵧ²). The principal stresses are C ± R, and the largest in-plane shear stress is R.

Transformation equation

σθ = −10 + 10·−0.1736 + 40·0.9848 = 27.66 MPa

Answer

σθ = 27.66 MPa
7.Axial stress & strain

Answer: P = 12.14 kN

Two materials: in series (one after the other) every segment carries the same force and the elongations add: δ = P·Σ L/(E·A). In parallel (side by side between rigid plates) both parts shorten by the same amount, so their strains are equal: the stiffer part takes the larger share, Pi = P·EiAi/ΣEA, and σi = Ei·ε. A bar held between two rigid walls with a load at the junction is statically indeterminate: the two segments share the load in proportion to their stiffness k = EA/L.

Areas

A₁ = 314.2 mm², A₂ = 706.9 mm²

Flexibilities

L₁/(E₁A₁) = 400/(200000·314.2) = 6.366 × 10⁻⁶ mm/N
L₂/(E₂A₂) = 500/(70000·706.9) = 1.011 × 10⁻⁵ mm/N

Load

P = 0.2/1.647 × 10⁻⁵ = 12142 N = 12.14 kN

Answer

P = 12.14 kN
8.Axial stress & strain

Answer: σ2 = 5.605 MPa

Two materials: in series (one after the other) every segment carries the same force and the elongations add: δ = P·Σ L/(E·A). In parallel (side by side between rigid plates) both parts shorten by the same amount, so their strains are equal: the stiffer part takes the larger share, Pi = P·EiAi/ΣEA, and σi = Ei·ε. A bar held between two rigid walls with a load at the junction is statically indeterminate: the two segments share the load in proportion to their stiffness k = EA/L.

Stiffnesses

k₁ = 200000·706.9/400 = 353429 N/mm
k₂ = 70000·2827/500 = 395841 N/mm

Share of segment 2

F2 = 30000·395841/749270 = 15849 N

Stress

σ2 = 15849/2827 = 5.605 MPa (compression)

Answer

σ2 = 5.605 MPa
9.Column buckling

Answer: Pcr = 71.19 kN

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·30⁴/64 = 39761 mm⁴

Effective length

KL = 0.7·1500 = 1050 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·39761/1050² = 71188 N = 71.19 kN

Answer

Pcr = 71.19 kN
10.Column buckling

Answer: d = 67.61 mm

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Required critical load

Pcr = n·P = 2.5·90000 = 225000 N
KL = 2·1500 = 3000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·225000·3000²/(π³·200000))^(1/4) = 67.61 mm

Answer

d = 67.61 mm

Check: the slenderness KL/r is 177.5, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: fd = 2.273 Hz

Free vibration of a mass–spring system: the undamped natural frequency is ωn = √(k/m) in rad/s, and fn = ωn/(2π) in Hz. A viscous damper c gives the damping ratio ζ = c/cc, with critical damping cc = 2·√(k·m) = 2·m·ωn. An underdamped system (ζ < 1) oscillates at ωd = ωn·√(1 − ζ²). Springs in parallel add, k = k₁ + k₂; springs in series add as reciprocals, 1/k = 1/k₁ + 1/k₂.

Undamped natural frequency

ωn = √(40000/100) = 20 rad/s
fn = 20/(2π) = 3.183 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 3.183·√(1 − 0.7²) = 2.273 Hz

Answer

fd = 2.273 Hz
12.Mechanical vibrations

Answer: fn = 2.297 Hz

Free vibration of a mass–spring system: the undamped natural frequency is ωn = √(k/m) in rad/s, and fn = ωn/(2π) in Hz. A viscous damper c gives the damping ratio ζ = c/cc, with critical damping cc = 2·√(k·m) = 2·m·ωn. An underdamped system (ζ < 1) oscillates at ωd = ωn·√(1 − ζ²). Springs in parallel add, k = k₁ + k₂; springs in series add as reciprocals, 1/k = 1/k₁ + 1/k₂.

Equivalent stiffness

Springs in series share the same force and add their deflections, so they combine as reciprocals: 1/k = 1/k1 + 1/k2.

1/keq = 1/50 + 1/10 → keq = 50·10/(50 + 10) = 8.333 kN/m

Natural frequency

ωn = √(8333/40) = 14.43 rad/s
fn = 14.43/(2π) = 2.297 Hz

Answer

fn = 2.297 Hz

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