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​ = 12N2​ = 18

A 7.5 kW motor running at 960 rpm drives a pinion with 12 teeth, which meshes with a gear with 18 teeth. The gear pair has an efficiency of 96%. Find the output torque T2 on the gear shaft.

P = 7.5 kWn1 = 960 rpmN1 = 12N2 = 18η = 96%
T2 = N·m
2.Gears & gear trainsHard
A = 12B = 80C = 40D = 72

In a compound gear train, gear A (12 teeth) on the input shaft turning at 3000 rpm drives gear B (80 teeth). Gear C (40 teeth) is fixed to the same shaft as B and drives gear D (72 teeth) on the output shaft. Find the output speed nout.

nin = 3000 rpmA = 12B = 80C = 40D = 72
nout = rpm
3.Torsion of shaftsMedium
T = 200 N·md = 20 mmL = 0.8 mφ = ?

A solid aluminium shaft is fixed at the wall and twisted by a torque T at its free end. Find the angle of twist φ of the free end, in degrees.

T = 200 N·md = 20 mmL = 0.8 mG = 26 GPa
φ = °
4.Torsion of shaftsHard
d = 30 mmTB​ = 1000 N·mTC​ = 250 N·mABC2 m1.5 m

A solid steel shaft of diameter 30 mm is fixed at A. A torque of 1000 N·m acts at B, 2 m from A, and a torque of 250 N·m in the same direction acts at the free end C, a further 1.5 m along. Find the maximum shear stress τmax in the shaft.

d = 30 mmTB = 1000 N·mTC = 250 N·mAB = 2 mBC = 1.5 m
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = 10σy​ = 100τxy​ = 30MPa

A point in a loaded part has σₓ = 10 MPa, σᵧ = 100 MPa and τₓᵧ = 30 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = 10 MPaσy = 100 MPaτxy = 30 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​ = 0σy​ = 50τxy​ = 30MPa

A point in a loaded part has σₓ = 0 MPa, σᵧ = 50 MPa and τₓᵧ = 30 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 30° clockwise from the x-axis.

σx = 0 MPaσy = 50 MPaτxy = 30 MPaθ = -30°
σθ = MPa
7.Axial stress & strainMedium
P = ?12300 mm200 mmØ30Ø60δ = 0.3 mm

A bar is made of a steel segment (diameter 30 mm, length 300 mm, E = 200 GPa) joined end to end with a segment made of copper (diameter 60 mm, length 200 mm, E = 120 GPa). It is fixed at one end and pulled at the other. Find the axial load P that stretches it by 0.3 mm in total.

segment 1: steel, Ø30 mm, 300 mm, E = 200 GPasegment 2: copper, Ø60 mm, 200 mm, E = 120 GPaδ = 0.3 mm
P = kN
8.Axial stress & strainHard
80 kN12400 mm200 mmØ30Ø30σ2​ = ?

A steel segment (diameter 30 mm, length 400 mm, E = 200 GPa) and a segment made of aluminium (diameter 30 mm, length 200 mm, E = 70 GPa) are joined end to end and fixed between two rigid walls. An axial load of 80 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, Ø30 mm, 200 mm, E = 70 GPaP = 80 kN
σ2 = MPa
9.Column bucklingMedium
PL = 6 m30 × 80 mmcross-section

A column of length L made of steel is fixed at both ends. Using Euler’s formula, find its critical buckling load Pcr.

L = 6 mE = 200 GPa (steel)b × h = 30 × 80 mm
Pcr = kN
10.Column bucklingHard
PL = 5 md = 40 mmcross-section

A column of length L made of steel is pinned at both ends. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 5 mE = 200 GPa (steel)d = 40 mm
σcr = MPa
11.Mechanical vibrationsMedium
tx10 mm3 cycles1.5 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 10 mm is followed 3 cycles later by a peak of 1.5 mm. Find the damping ratio ζ.

x0 = 10 mmx3 = 1.5 mmn = 3
ζ =
12.Mechanical vibrationsHard
k1​ = 30k2​ = 25k3​ = 40m = 20 kg

A 20 kg mass hangs from spring k₃ = 40 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 30 kN/m and k₂ = 25 kN/m; the bar stays level. Ignore damping and the masses of the springs and bar. Find the natural frequency fn of vertical vibration in Hz.

m = 20 kgk1 = 30 kN/mk2 = 25 kN/mk3 = 40 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: T2 = 107.4 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·960/60 = 100.5 rad/s
T1 = P/ω₁ = 7500/100.5 = 74.6 N·m

Output torque

T2 = 74.6·18/12·0.96 = 107.4 N·m

Answer

T2 = 107.4 N·m
2.Gears & gear trains

Answer: nout = 250 rpm

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.

First stage

nB = 3000·12/80 = 450 rpm = nC

Second stage

nout = 450·40/72 = 250 rpm

Answer

nout = 250 rpm

total ratio = 12 : 1

3.Torsion of shafts

Answer: φ = 22.45 °

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 second moment of area

J = π·20⁴/32 = 15708 mm⁴

Angle of twist

φ = TL/(GJ) = 200·1000·800/(26000·15708) = 0.3918 rad
φ = 0.3918·180/π = 22.45°

Answer

φ = 22.45°
4.Torsion of shafts

Answer: τmax = 235.8 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 = 250 N·m
TAB = TC + TB = 250 + 1000 = 1250 N·m

Maximum shear stress

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

|T|max = 1250 N·m
τmax = 16·1.25 × 10⁶/(π·30³) = 235.8 MPa

Answer

τmax = 235.8 MPa
5.Mohr’s circle & stress transformation

Answer: θp = 73.15 °

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.

στxyCσ1​σ2​

Angle on the circle

Point x sits at an angle 2θp from the σ-axis on Mohr’s circle; the quadrant follows from the signs of σₓ − σᵧ and τₓᵧ.

2θp = atan2(2·30, 10 − 100) = 146.3°

Angle on the element

θp = 73.15°

Answer

θp = 73.15°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: σθ = −13.48 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 = 25 + −25·0.5 + 30·−0.866 = −13.48 MPa

Answer

σθ = −13.48 MPa
7.Axial stress & strain

Answer: P = 110.6 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 = 706.9 mm², A₂ = 2827 mm²

Flexibilities

L₁/(E₁A₁) = 300/(200000·706.9) = 2.122 × 10⁻⁶ mm/N
L₂/(E₂A₂) = 200/(120000·2827) = 5.895 × 10⁻⁷ mm/N

Load

P = 0.3/2.712 × 10⁻⁶ = 110639 N = 110.6 kN

Answer

P = 110.6 kN
8.Axial stress & strain

Answer: σ2 = 46.6 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 = 70000·706.9/200 = 247400 N/mm

Share of segment 2

F2 = 80000·247400/600830 = 32941 N

Stress

σ2 = 32941/706.9 = 46.6 MPa (compression)

Answer

σ2 = 46.6 MPa
9.Column buckling

Answer: Pcr = 39.48 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 = 80·30³/12 = 180000 mm⁴

Effective length

KL = 0.5·6000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·180000/3000² = 39478 N = 39.48 kN

Answer

Pcr = 39.48 kN
10.Column buckling

Answer: σcr = 7.896 MPa

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·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 1·5000 = 5000 mm
KL/r = 5000/10 = 500

Critical stress

σcr = π²E/(KL/r)² = π²·200000/500² = 7.896 MPa

Answer

σcr = 7.896 MPa
11.Mechanical vibrations

Answer: ζ = 0.1001

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.

Logarithmic decrement

δ = (1/3)·ln(10/1.5) = 0.6324

Damping ratio

ζ = δ/√(4π² + δ²) = 0.6324/√(39.48 + 0.3999) = 0.1001

Answer

ζ = 0.1001
12.Mechanical vibrations

Answer: fn = 5.416 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

Only k1 and k2 are in parallel. That pair is in series with k3, so combine them as reciprocals.

k12 = 30 + 25 = 55 kN/m
keq = 55·40/(55 + 40) = 23.16 kN/m

Natural frequency

ωn = √(23158/20) = 34.03 rad/s
fn = 34.03/(2π) = 5.416 Hz

Answer

fn = 5.416 Hz

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