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​ = 30N2​ = 40

A 1.5 kW motor running at 1500 rpm drives a pinion with 30 teeth, which meshes with a gear with 40 teeth. Ignore losses. Find the torque T1 on the motor shaft.

P = 1.5 kWn1 = 1500 rpmN1 = 30N2 = 40η = 100%
T1 = N·m
2.Gears & gear trainsHard
A = 48B = 60C = 24D = ?

In a compound gear train, gear A (48 teeth) on the input shaft turns at 1450 rpm and drives gear B (60 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 348 rpm. How many teeth ND must gear D have?

nin = 1450 rpmA = 48B = 60C = 24nout = 348 rpm
ND =
3.Torsion of shaftsMedium
d = ?T = 1000 N·mL = 1.5 m

A solid steel shaft 1.5 m long carries a torque of 1000 N·m. The angle of twist between its ends must not exceed 1°. Find the smallest diameter d that meets this limit.

T = 1000 N·mL = 1.5 mG = 80 GPaφallow = 1°
d = mm
4.Torsion of shaftsHard
Tdo​ = 40 mm, di​ = 32 mm

A hollow shaft transmits 10 kW at 500 rpm. Find the maximum shear stress τmax in the shaft.

P = 10 kWN = 500 rpmdo = 40 mmdi = 32 mm
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = 60σy​ = 10MPaτxy​ = ?

A point has σₓ = 60 MPa and σᵧ = 10 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 120 MPa?

σx = 60 MPaσy = 10 MPaσ1 = 120 MPa
τxy = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 20σy​ = 90τxy​ = 10MPa

A point in a thin plate is in plane stress: σₓ = 20 MPa, σᵧ = 90 MPa and τₓᵧ = 10 MPa (σz = 0). Find the von Mises equivalent stress σvM.

σx = 20 MPaσy = 90 MPaτxy = 10 MPa
σvM = MPa
7.Axial stress & strainMedium
Ø 25 mmAluminium2.5 mP = 120 kN

Find the axial strain ε in the aluminium bar, in microstrain (µε = 10⁻⁶).

P = 120 kNd = 25 mmL = 2.5 mE = 70 GPa
ε = µε
8.Axial stress & strainHard
Ø 25 mmAluminium0.5 mØ 12 mmCopper2 mP = 15 kN

The stepped bar is fixed at the wall and loaded at its free end. Find the largest normal stress σmax in the bar.

P = 15 kNsegment 1: Ø25 mm, 0.5 m, aluminium (E = 70 GPa)segment 2: Ø12 mm, 2 m, copper (E = 117 GPa)
σmax = MPa
9.Column bucklingMedium
PL = 1.5 m50 × 60 mmcross-section

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

L = 1.5 mE = 70 GPa (aluminium)b × h = 50 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 80 kNL = 2.5 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and pinned at the top. It must carry 80 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 80 kNn = 2L = 2.5 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
k = 40 kN/mc = 230 N·s/mm = 2 kg

A 2 kg mass is supported by a spring with a stiffness of 40 kN/m and a viscous damper with a damping coefficient of 230 N·s/m. Find the damping ratio ζ.

m = 2 kgk = 40 kN/mc = 230 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 30k2​ = 20m = 10 kg

A 10 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 30 kN/m and k₂ = 20 kN/m. The mass stays level. Find the equivalent stiffness keq of the spring system in kN/m.

m = 10 kgk1 = 30 kN/mk2 = 20 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: T1 = 9.549 N·m

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.

Motor torque

ω₁ = 2π·1500/60 = 157.1 rad/s
T1 = P/ω₁ = 1500/157.1 = 9.549 N·m

Answer

T1 = 9.549 N·m
2.Gears & gear trains

Answer: ND = 80

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 = 1450·48/60 = 1160 rpm

Teeth on gear D

ND = C·nC/nout = 24·1160/348 = 80

Answer

ND = 80
3.Torsion of shafts

Answer: d = 57.51 mm

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.

Required polar moment

T = 1000 N·m = 1 × 10⁶ N·mm
L = 1.5 m = 1500 mm
G = 80 GPa = 80000 MPa
φ = 1·π/180 = 0.01745 rad
J = TL/(Gφ) = 1 × 10⁶·1500/(80000·0.01745) = 1.074 × 10⁶ mm⁴

Diameter

d = (32J/π)1/4 = 57.51 mm

Answer

d = 57.51 mm

In practice you would round up to the next standard size.

4.Torsion of shafts

Answer: τmax = 25.74 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.

Torque

ω = 2πN/60 = 2π·500/60 = 52.36 rad/s
T = P/ω = 10000/52.36 = 191 N·m

Polar second moment of area

J = π(40⁴ − 32⁴)/32 = 148384 mm⁴

Maximum shear stress

τmax = T·(do/2)/J = 190986·20/148384 = 25.74 MPa

Answer

τmax = 25.74 MPa
5.Mohr’s circle & stress transformation

Answer: τxy = 81.24 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.

Required radius

C = (60 + 10)/2 = 35 MPa
R = σ1 − C = 120 − 35 = 85 MPa
στxyCσ1​σ2​

Shear stress

τxy = √(R² − ((σₓ − σᵧ)/2)²) = √(85² − 25²) = 81.24 MPa

Answer

τxy = 81.24 MPa
6.Mohr’s circle & stress transformation

Answer: σvM = 83.67 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. Yield criteria: von Mises predicts yield when σvM = √(σ₁² − σ₁σ₂ + σ₂²) reaches σY; Tresca when the absolute maximum shear stress reaches σY/2.

στxyCσ1​σ2​

Principal stresses

C = 55 MPa, R = 36.4 MPa
σ1 = 91.4 MPa, σ2 = 18.6 MPa, σ3 = 0

Von Mises

σvM = √(91.4² − 91.4·18.6 + 18.6²) = 83.67 MPa

Answer

σvM = 83.67 MPa
7.Axial stress & strain

Answer: ε = 3492 µε

Hooke’s law: within the elastic range σ = E·ε. Combining with σ = P/A and ε = δ/L gives δ = PL/(AE).

Stress

A = π·25²/4 = 490.9 mm²
σ = P/A = 120·1000/490.9 = 244.5 MPa

Strain (Hooke’s law)

E for aluminium = 70 GPa = 70000 MPa.

ε = σ/E = 244.5/70000 = 0.003492 = 3492 µε

Answer

ε = 3492 µε
8.Axial stress & strain

Answer: σmax = 132.6 MPa

Axially loaded members: each prismatic segment obeys δ = PL/(AE). For members in series the elongations add.

Same force in both segments

The free end carries P, so every section of the bar carries the same axial force P. Only the areas and materials change.

A1 = π·25²/4 = 490.9 mm², A2 = π·12²/4 = 113.1 mm²
σ1 = 30.56 MPa
σ2 = 132.6 MPa

Largest stress

The thinner segment has the smaller area, so it carries the larger stress.

σmax = 132.6 MPa

Answer

σmax = 132.6 MPa
9.Column buckling

Answer: Pcr = 47.98 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 rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 60·50³/12 = 625000 mm⁴

Effective length

KL = 2·1500 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·625000/3000² = 47977 N = 47.98 kN

Answer

Pcr = 47.98 kN
10.Column buckling

Answer: d = 47.42 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 = 2·80000 = 160000 N
KL = 0.7·2500 = 1750 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·160000·1750²/(π³·200000))^(1/4) = 47.42 mm

Answer

d = 47.42 mm

Check: the slenderness KL/r is 147.6, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.4066

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.

Critical damping

cc = 2·√(k·m) = 2·√(40000·2) = 565.7 N·s/m

Damping ratio

ζ = c/cc = 230/565.7 = 0.4066

Answer

ζ = 0.4066

ζ < 1, so the system is underdamped and oscillates as it decays.

12.Mechanical vibrations

Answer: keq = 50 kN/m

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 side by side share the deflection and add their forces, so their stiffnesses simply add: k = k1 + k2.

keq = 30 + 20 = 50 kN/m

Answer

keq = 50 kN/m

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