Machine Design: cram pack

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

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

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​ = 25, m = 2 mm

An 11 kW motor running at 1440 rpm drives a pinion with 25 teeth and a module of 2 mm. Find the tangential force Ft on the pinion teeth.

P = 11 kWn = 1440 rpmN1 = 25m = 2 mm
Ft = N
2.Gears & gear trainsHard
A = 25B = 30C = 18D = 50

In a compound gear train, gear A (25 teeth) on the input shaft turning at 1500 rpm drives gear B (30 teeth). Gear C (18 teeth) is fixed to the same shaft as B and drives gear D (50 teeth) on the output shaft. Find the output speed nout.

nin = 1500 rpmA = 25B = 30C = 18D = 50
nout = rpm
3.Torsion of shaftsMedium
d = 20 mmT = 100 N·m400 mmφ = 3.74°

In a torsion test, a solid specimen of diameter 20 mm is twisted by a torque of 100 N·m. The two ends of a gauge length of 400 mm rotate 3.74° relative to each other (the material is still elastic). Find the shear modulus G of the material.

T = 100 N·md = 20 mmL = 400 mmφ = 3.74°
G = GPa
4.Torsion of shaftsHard
do​ = ?75 kW, 1500 rpm

A hollow shaft must transmit 75 kW at 1500 rpm. Its inner diameter is to be 0.5 times its outer diameter, and the shear stress must not exceed 75 MPa. Find the smallest outer diameter do.

P = 75 kWN = 1500 rpmdi/do = 0.5τallow = 75 MPa
do = mm
5.Mohr’s circle & stress transformationMedium
σx​ = −30σy​ = 0τxy​ = 10MPa

A point in a loaded part has σₓ = −30 MPa, σᵧ = 0 MPa and τₓᵧ = 10 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = −30 MPaσy = 0 MPaτxy = 10 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​τxy​surface of the shaft

A solid shaft of diameter 40 mm carries an axial compressive force of 80 kN together with a torque of 1500 N·m. At the surface of the shaft, find the largest principal stress σ1.

d = 40 mmF = −80 kNT = 1500 N·m
σ1 = MPa
7.Axial stress & strainMedium
50 kNØ2070 GPaØ100/50600 mmδ = ?

A steel rod (diameter 20 mm, E = 200 GPa) sits inside a tube made of aluminium (outer diameter 100 mm, inner diameter 50 mm, E = 70 GPa). Both are 600 mm long and are compressed together between rigid plates by 50 kN. Find the shortening δ.

P = 50 kNrod: Ø20 mm, E = 200 GPatube: Ø100/Ø50 mm, E = 70 GPaL = 600 mm
δ = mm
8.Axial stress & strainHard
P = ?Ø2070 GPaØ100/70600 mm

A steel rod (diameter 20 mm, E = 200 GPa, allowable stress 150 MPa) sits inside a tube made of aluminium (outer diameter 100 mm, inner diameter 70 mm, E = 70 GPa, allowable stress 60 MPa). They are compressed together between rigid plates. Find the largest load Pmax.

rod: Ø20 mm, E = 200 GPa, σallow = 150 MPatube: Ø100/Ø70 mm, E = 70 GPa, σallow = 60 MPa
Pmax = kN
9.Column bucklingMedium
PL = 2.5 m40 × 60 mmcross-section

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

L = 2.5 mE = 200 GPa (steel)b × h = 40 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 105 kNL = 3 md = ?cross-section

A solid round column of length L made of aluminium is fixed at both ends. It must carry 105 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 105 kNn = 2.5L = 3 mE = 70 GPa (aluminium)
d = mm
11.Mechanical vibrationsMedium
tx40 mm3 cycles18.8 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 40 mm is followed 3 cycles later by a peak of 18.8 mm. Find the damping ratio ζ.

x0 = 40 mmx3 = 18.8 mmn = 3
ζ =
12.Mechanical vibrationsHard
k1​ = 12k2​ = 100k3​ = 40m = 100 kg

A 100 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 = 12 kN/m and k₂ = 100 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 = 100 kgk1 = 12 kN/mk2 = 100 kN/mk3 = 40 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: Ft = 2918 N

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.

Torque on the pinion

ω = 2π·1440/60 = 150.8 rad/s
T = P/ω = 11000/150.8 = 72.95 N·m

Pitch diameter

d = m·N = 2·25 = 50 mm

Tangential force

Ft = 2T/d = 2·72.95/0.05 = 2918 N

Answer

Ft = 2918 N
2.Gears & gear trains

Answer: nout = 450 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 = 1500·25/30 = 1250 rpm = nC

Second stage

nout = 1250·18/50 = 450 rpm

Answer

nout = 450 rpm

total ratio = 3.333 : 1

3.Torsion of shafts

Answer: G = 39.01 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 = 3.74·π/180 = 0.06528 rad

Shear modulus

T = 100 N·m = 100000 N·mm
G = TL/(Jφ) = 100000·400/(15708·0.06528) = 39011 MPa
G = 39.01 GPa

Answer

G = 39.01 GPa

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

4.Torsion of shafts

Answer: do = 32.58 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.

Torque

ω = 2πN/60 = 2π·1500/60 = 157.1 rad/s
T = P/ω = 75000/157.1 = 477.5 N·m

Outer diameter from the allowable stress

T = 477.5 N·m = 477465 N·mm
1 − k⁴ = 1 − 0.5⁴ = 0.9375
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·477465/(π·75·0.9375)) = 32.58 mm
di = 0.5·32.58 = 16.29 mm

Answer

do = 32.58 mm

A solid shaft would need d = 31.89 mm; the hollow one is a little larger but much lighter.

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(2·10, −30 − 0) = 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: σ1 = 91.71 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.

Stresses at the surface

σ = F/A = −80000/(π·40²/4) = −80000/1257 = −63.66 MPa
τ = 16T/(πd³) = 16·1500000/(π·40³) = 119.4 MPa
στxyCσ1​σ2​

Mohr’s circle

C = σ/2 = −31.83 MPa
R = √((−31.83)² + 119.4²) = 123.5 MPa
σ1 = C + R = 91.71 MPa
σ2 = C − R = −155.4 MPa

Answer

σ1 = 91.71 MPa
7.Axial stress & strain

Answer: δ = 0.06314 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·20²/4 = 314.2 mm²
At = π(100² − 50²)/4 = 5890 mm²

Combined axial stiffness

ΣEA = 200·10³·314.2 + 70·10³·5890 = 4.752 × 10⁸ N

Shortening

δ = 50000·600/4.752 × 10⁸ = 0.06314 mm

Answer

δ = 0.06314 mm
8.Axial stress & strain

Answer: Pmax = 257.4 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

Ar = π·20²/4 = 314.2 mm²
At = π(100² − 70²)/4 = 4006 mm²

Combined axial stiffness

ΣEA = 200·10³·314.2 + 70·10³·4006 = 3.432 × 10⁸ N

Governing strain

ε = min(0.00075, 0.0008571) = 0.00075 (steel)

Largest load

Pmax = 0.00075·3.432 × 10⁸ = 257414 N = 257.4 kN

Answer

Pmax = 257.4 kN
9.Column buckling

Answer: Pcr = 101.1 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 = 60·40³/12 = 320000 mm⁴

Effective length

KL = 1·2500 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·320000/2500² = 101065 N = 101.1 kN

Answer

Pcr = 101.1 kN
10.Column buckling

Answer: d = 64.6 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 = 2.5·105000 = 262500 N
KL = 0.5·3000 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·262500·1500²/(π³·70000))^(1/4) = 64.6 mm

Answer

d = 64.6 mm

Check: the slenderness KL/r is 92.88, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.04002

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(40/18.8) = 0.2517

Damping ratio

ζ = δ/√(4π² + δ²) = 0.2517/√(39.48 + 0.06334) = 0.04002

Answer

ζ = 0.04002
12.Mechanical vibrations

Answer: fn = 2.732 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 = 12 + 100 = 112 kN/m
keq = 112·40/(112 + 40) = 29.47 kN/m

Natural frequency

ωn = √(29474/100) = 17.17 rad/s
fn = 17.17/(2π) = 2.732 Hz

Answer

fn = 2.732 Hz

ExamProblems · examproblems.com/courses/machine-design