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 100 mm apart. They must be connected by a pair of spur gears with a module of 2 mm and a speed reduction of 4 : 1. How many teeth N2 must the gear have?

a = 100 mmm = 2 mmi = 4
N2 =
2.Gears & gear trainsHard
A = 36B = 80C = 16D = 20

In a compound gear train, gear A (36 teeth) on the input shaft turning at 1440 rpm drives gear B (80 teeth). Gear C (16 teeth) is fixed to the same shaft as B and drives gear D (20 teeth) on the output shaft. Find the output speed nout.

nin = 1440 rpmA = 36B = 80C = 16D = 20
nout = rpm
3.Torsion of shaftsMedium
d1​ = 30 mmd2​ = 25 mmT = 100 N·mABC2.5 m0.5 m

A stepped solid steel shaft is fixed at A. Segment AB has diameter 30 mm and length 2.5 m; segment BC has diameter 25 mm and length 0.5 m. A torque of 100 N·m acts at the free end C. Find the maximum shear stress τmax in the shaft.

T = 100 N·md1 = 30 mm, L1 = 2.5 md2 = 25 mm, L2 = 0.5 m
τmax = MPa
4.Torsion of shaftsHard
d = 50 mmTB​ = 200 N·mTC​ = 250 N·mABC1.2 m0.5 m

A solid brass shaft of diameter 50 mm is fixed at A. A torque of 200 N·m acts at B, 1.2 m from A, and a torque of 250 N·m in the same direction acts at the free end C, a further 0.5 m along. Find the magnitude of the angle of twist φC of end C, in degrees.

d = 50 mmTB = 200 N·mTC = 250 N·mAB = 1.2 mBC = 0.5 mG = 39 GPa
φC = °
5.Mohr’s circle & stress transformationMedium
σx​ = −40σy​ = 20MPaτxy​ = ?

A point has σₓ = −40 MPa and σᵧ = 20 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 60 MPa?

σx = −40 MPaσy = 20 MPaσ1 = 60 MPa
τxy = MPa
6.Mohr’s circle & stress transformationHard
σx​ = −80σy​ = 50τxy​ = −30MPa

A point in a loaded part has σₓ = −80 MPa, σᵧ = 50 MPa and τₓᵧ = −30 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 60° counter-clockwise from the x-axis.

σx = −80 MPaσy = 50 MPaτxy = −30 MPaθ = 60°
σθ = MPa
7.Axial stress & strainMedium
50 kNØ25110 GPaØ100/70600 mmδ = ?

A steel rod (diameter 25 mm, E = 200 GPa) sits inside a tube made of bronze (outer diameter 100 mm, inner diameter 70 mm, E = 110 GPa). Both are 600 mm long and are compressed together between rigid plates by 50 kN. Find the shortening δ.

P = 50 kNrod: Ø25 mm, E = 200 GPatube: Ø100/Ø70 mm, E = 110 GPaL = 600 mm
δ = mm
8.Axial stress & strainHard
40 kN12600 mm500 mmØ20Ø30σ2​ = ?

A steel segment (diameter 20 mm, length 600 mm, E = 200 GPa) and a segment made of brass (diameter 30 mm, length 500 mm, E = 100 GPa) are joined end to end and fixed between two rigid walls. An axial load of 40 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø20 mm, 600 mm, E = 200 GPasegment 2: brass, Ø30 mm, 500 mm, E = 100 GPaP = 40 kN
σ2 = MPa
9.Column bucklingMedium
PL = 2 md = 40 mmcross-section

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

L = 2 mE = 70 GPa (aluminium)d = 40 mm
Pcr = kN
10.Column bucklingHard
P = 75 kNL = 4 md = ?cross-section

A solid round column of length L made of aluminium is pinned at both ends. It must carry 75 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 75 kNn = 3L = 4 mE = 70 GPa (aluminium)
d = mm
11.Mechanical vibrationsMedium
k = 50 kN/mζ = 0.3m = 12 kg

A 12 kg mass on a spring with a stiffness of 50 kN/m has a viscous damper giving a damping ratio of 0.3. Find the damped natural frequency fd of its free vibration in Hz.

m = 12 kgk = 50 kN/mζ = 0.3
fd = Hz
12.Mechanical vibrationsHard
k1​ = 25k2​ = 15m = 10 kg

A 10 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 25 kN/m and k₂ = 15 kN/m. The mass stays level. Ignore damping and the masses of the springs. Find the natural frequency fn of vertical vibration in Hz.

m = 10 kgk1 = 25 kN/mk2 = 15 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: N2 = 80

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 = 2·100/2 = 100

Split by the ratio

N1 = 100/(1 + 4) = 20
N2 = 4·20 = 80

Answer

N2 = 80
2.Gears & gear trains

Answer: nout = 518.4 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 = 1440·36/80 = 648 rpm = nC

Second stage

nout = 648·16/20 = 518.4 rpm

Answer

nout = 518.4 rpm

total ratio = 2.778 : 1

3.Torsion of shafts

Answer: τmax = 32.59 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.

Stress in each segment

T = 100 N·m = 100000 N·mm
τAB = 16·100000/(π·30³) = 18.86 MPa
τBC = 16·100000/(π·25³) = 32.59 MPa

Answer

τmax = 32.59 MPa
4.Torsion of shafts

Answer: φC = 1.592 °

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 + 200 = 450 N·m

Twist of each segment

J = π·50⁴/32 = 613592 mm⁴
G = 39 GPa = 39000 MPa
φAB = 450000·1200/(39000·613592) = 0.02257 rad
φBC = 250000·500/(39000·613592) = 0.005224 rad

Twist of end C

φC = 0.02257 + 0.005224 = 0.02779 rad → |φC| = 1.592°

Answer

φC = 1.592°
5.Mohr’s circle & stress transformation

Answer: τxy = 63.25 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 = (−40 + 20)/2 = −10 MPa
R = σ1 − C = 60 − (−10) = 70 MPa
στxyCσ1​σ2​

Shear stress

τxy = √(R² − ((σₓ − σᵧ)/2)²) = √(70² − 30²) = 63.25 MPa

Answer

τxy = 63.25 MPa
6.Mohr’s circle & stress transformation

Answer: σθ = −8.481 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 = −15 + −65·−0.5 + −30·0.866 = −8.481 MPa

Answer

σθ = −8.481 MPa
7.Axial stress & strain

Answer: δ = 0.05568 mm

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

Ar = π·25²/4 = 490.9 mm²
At = π(100² − 70²)/4 = 4006 mm²

Combined axial stiffness

ΣEA = 200·10³·490.9 + 110·10³·4006 = 5.388 × 10⁸ N

Shortening

δ = 50000·600/5.388 × 10⁸ = 0.05568 mm

Answer

δ = 0.05568 mm
8.Axial stress & strain

Answer: σ2 = 32.51 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 = 200000·314.2/600 = 104720 N/mm
k₂ = 100000·706.9/500 = 141372 N/mm

Share of segment 2

F2 = 40000·141372/246091 = 22979 N

Stress

σ2 = 22979/706.9 = 32.51 MPa (compression)

Answer

σ2 = 32.51 MPa
9.Column buckling

Answer: Pcr = 44.29 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·40⁴/64 = 125664 mm⁴

Effective length

KL = 0.7·2000 = 1400 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·125664/1400² = 44295 N = 44.29 kN

Answer

Pcr = 44.29 kN
10.Column buckling

Answer: d = 101.5 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 = 3·75000 = 225000 N
KL = 1·4000 = 4000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·225000·4000²/(π³·70000))^(1/4) = 101.5 mm

Answer

d = 101.5 mm

Check: the slenderness KL/r is 157.6, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: fd = 9.8 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 = √(50000/12) = 64.55 rad/s
fn = 64.55/(2π) = 10.27 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 10.27·√(1 − 0.3²) = 9.8 Hz

Answer

fd = 9.8 Hz
12.Mechanical vibrations

Answer: fn = 10.07 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 side by side share the deflection and add their forces, so their stiffnesses simply add: k = k1 + k2.

keq = 25 + 15 = 40 kN/m

Natural frequency

ωn = √(40000/10) = 63.25 rad/s
fn = 63.25/(2π) = 10.07 Hz

Answer

fn = 10.07 Hz

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