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​ = 32

A 2.2 kW motor running at 1450 rpm drives a pinion with 12 teeth, which meshes with a gear with 32 teeth. Ignore losses. Find the output torque T2 on the gear shaft.

P = 2.2 kWn1 = 1450 rpmN1 = 12N2 = 32η = 100%
T2 = N·m
2.Gears & gear trainsHard
A = 16B = 32C = 48D = 60

In a compound gear train, gear A (16 teeth) on the input shaft turning at 1440 rpm drives gear B (32 teeth). Gear C (48 teeth) is fixed to the same shaft as B and drives gear D (60 teeth) on the output shaft. Find the output speed nout.

nin = 1440 rpmA = 16B = 32C = 48D = 60
nout = rpm
3.Torsion of shaftsMedium
T = 250 N·md = 50 mmL = 1.2 mφ = ?

A solid steel 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 = 250 N·md = 50 mmL = 1.2 mG = 80 GPa
φ = °
4.Torsion of shaftsHard
do​ = ?30 kW, 500 rpm

A hollow shaft must transmit 30 kW at 500 rpm. Its inner diameter is to be 0.75 times its outer diameter, and the shear stress must not exceed 75 MPa. Find the smallest outer diameter do.

P = 30 kWN = 500 rpmdi/do = 0.75τallow = 75 MPa
do = mm
5.Mohr’s circle & stress transformationMedium
σx​ = −60σy​ = 60τxy​ = 10MPa

A point in a loaded part has σₓ = −60 MPa, σᵧ = 60 MPa and τₓᵧ = 10 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = −60 MPaσy = 60 MPaτxy = 10 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 50σy​ = −20τxy​ = 50MPa

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

σx = 50 MPaσy = −20 MPaτxy = 50 MPaθ = -20°
σθ = MPa
7.Axial stress & strainMedium
Ø 20 mmSteel1.5 mP = 30 kN

Find the elongation δ of the steel bar under the axial load.

P = 30 kNd = 20 mmL = 1.5 mE = 200 GPa
δ = mm
8.Axial stress & strainHard
Ø 25 mmAluminium2 mØ 20 mmCopper1 mP = 25 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 = 25 kNsegment 1: Ø25 mm, 2 m, aluminium (E = 70 GPa)segment 2: Ø20 mm, 1 m, copper (E = 117 GPa)
σmax = MPa
9.Column bucklingMedium
PL = 1 md = 60 mmcross-section

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

L = 1 mE = 200 GPa (steel)d = 60 mm
Pcr = kN
10.Column bucklingHard
P = 20 kNL = 2 md = ?cross-section

A solid round column of length L made of aluminium is pinned at both ends. It must carry 20 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 20 kNn = 2.5L = 2 mE = 70 GPa (aluminium)
d = mm
11.Mechanical vibrationsMedium
k = 50 kN/mζ = 0.45m = 50 kg

A 50 kg mass on a spring with a stiffness of 50 kN/m has a viscous damper giving a damping ratio of 0.45. Find the damped natural frequency fd of its free vibration in Hz.

m = 50 kgk = 50 kN/mζ = 0.45
fd = Hz
12.Mechanical vibrationsHard
k1​ = 100k2​ = 100m = 25 kg

A 25 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 100 kN/m and k₂ = 100 kN/m. The mass stays level. Find the equivalent stiffness keq of the spring system in kN/m.

m = 25 kgk1 = 100 kN/mk2 = 100 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: T2 = 38.64 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·1450/60 = 151.8 rad/s
T1 = P/ω₁ = 2200/151.8 = 14.49 N·m

Output torque

T2 = 14.49·32/12·1 = 38.64 N·m

Answer

T2 = 38.64 N·m
2.Gears & gear trains

Answer: nout = 576 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 = 1440·16/32 = 720 rpm = nC

Second stage

nout = 720·48/60 = 576 rpm

Answer

nout = 576 rpm

total ratio = 2.5 : 1

3.Torsion of shafts

Answer: φ = 0.3502 °

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·50⁴/32 = 613592 mm⁴

Angle of twist

φ = TL/(GJ) = 250·1000·1200/(80000·613592) = 0.006112 rad
φ = 0.006112·180/π = 0.3502°

Answer

φ = 0.3502°
4.Torsion of shafts

Answer: do = 38.47 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·500/60 = 52.36 rad/s
T = P/ω = 30000/52.36 = 573 N·m

Outer diameter from the allowable stress

T = 573 N·m = 572958 N·mm
1 − k⁴ = 1 − 0.75⁴ = 0.6836
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·572958/(π·75·0.6836)) = 38.47 mm
di = 0.75·38.47 = 28.85 mm

Answer

do = 38.47 mm

A solid shaft would need d = 33.89 mm; the hollow one is a little larger but much lighter.

5.Mohr’s circle & stress transformation

Answer: τmax = 60.83 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 = √(((−60 − 60)/2)² + 10²) = 60.83 MPa

Answer

τmax = 60.83 MPa
6.Mohr’s circle & stress transformation

Answer: σθ = 9.672 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 + 35·0.766 + 50·−0.6428 = 9.672 MPa

Answer

σθ = 9.672 MPa
7.Axial stress & strain

Answer: δ = 0.7162 mm

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·20²/4 = 314.2 mm²
σ = P/A = 30·1000/314.2 = 95.49 MPa

Strain (Hooke’s law)

E for steel = 200 GPa = 200000 MPa.

ε = σ/E = 95.49/200000 = 0.0004775 = 477.5 µε

Elongation

δ = ε·L = 0.0004775·1500 mm = 0.7162 mm

Answer

δ = 0.7162 mm
8.Axial stress & strain

Answer: σmax = 79.58 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·20²/4 = 314.2 mm²
σ1 = 50.93 MPa
σ2 = 79.58 MPa

Largest stress

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

σmax = 79.58 MPa

Answer

σmax = 79.58 MPa
9.Column buckling

Answer: Pcr = 313.9 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·60⁴/64 = 636173 mm⁴

Effective length

KL = 2·1000 = 2000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·636173/2000² = 313939 N = 313.9 kN

Answer

Pcr = 313.9 kN
10.Column buckling

Answer: d = 49.28 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 = 2.5·20000 = 50000 N
KL = 1·2000 = 2000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·50000·2000²/(π³·70000))^(1/4) = 49.28 mm

Answer

d = 49.28 mm

Check: the slenderness KL/r is 162.3, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: fd = 4.495 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 = √(50000/50) = 31.62 rad/s
fn = 31.62/(2π) = 5.033 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 5.033·√(1 − 0.45²) = 4.495 Hz

Answer

fd = 4.495 Hz
12.Mechanical vibrations

Answer: keq = 200 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 = 100 + 100 = 200 kN/m

Answer

keq = 200 kN/m

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