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​ = 16, m = 4 mm

A 15 kW motor running at 960 rpm drives a pinion with 16 teeth and a module of 4 mm. Find the tangential force Ft on the pinion teeth.

P = 15 kWn = 960 rpmN1 = 16m = 4 mm
Ft = N
2.Gears & gear trainsHard
A = 15B = 40C = 20D = 48

In a compound gear train, gear A (15 teeth) on the input shaft turning at 1500 rpm drives gear B (40 teeth). Gear C (20 teeth) is fixed to the same shaft as B and drives gear D (48 teeth) on the output shaft. Find the output speed nout.

nin = 1500 rpmA = 15B = 40C = 20D = 48
nout = rpm
3.Torsion of shaftsMedium
do​ = 40, di​ = 24 mmT = 400 N·mL = 1 m

A hollow aluminium shaft (outer diameter 40 mm, inner diameter 24 mm, length 1 m) is fixed at one end and twisted by a torque of 400 N·m at the other. Find the angle of twist φ in degrees.

T = 400 N·mdo = 40 mmdi = 24 mmL = 1 mG = 26 GPa
φ = °
4.Torsion of shaftsHard
do​ = ?5 kW, 3000 rpm

A hollow shaft must transmit 5 kW at 3000 rpm. Its inner diameter is to be 0.6 times its outer diameter, and the shear stress must not exceed 50 MPa. Find the smallest outer diameter do.

P = 5 kWN = 3000 rpmdi/do = 0.6τallow = 50 MPa
do = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 20σy​ = 30τxy​ = −50MPa

A point in a loaded part has σₓ = 20 MPa, σᵧ = 30 MPa and τₓᵧ = −50 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = 20 MPaσy = 30 MPaτxy = −50 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​ = 120σy​ = −10τxy​ = 40MPa

A point in a loaded part has σₓ = 120 MPa, σᵧ = −10 MPa and τₓᵧ = 40 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 30° clockwise from the x-axis (positive in the same sense as τₓᵧ).

σx = 120 MPaσy = −10 MPaτxy = 40 MPaθ = -30°
τθ = MPa
7.Axial stress & strainMedium
P = ?12400 mm400 mmØ40Ø30δ = 0.5 mm

A bar is made of a steel segment (diameter 40 mm, length 400 mm, E = 200 GPa) joined end to end with a segment made of bronze (diameter 30 mm, length 400 mm, E = 110 GPa). It is fixed at one end and pulled at the other. Find the axial load P that stretches it by 0.5 mm in total.

segment 1: steel, Ø40 mm, 400 mm, E = 200 GPasegment 2: bronze, Ø30 mm, 400 mm, E = 110 GPaδ = 0.5 mm
P = kN
8.Axial stress & strainHard
60 kN12300 mm500 mmØ30Ø60σ2​ = ?

A steel segment (diameter 30 mm, length 300 mm, E = 200 GPa) and a segment made of bronze (diameter 60 mm, length 500 mm, E = 110 GPa) are joined end to end and fixed between two rigid walls. An axial load of 60 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø30 mm, 300 mm, E = 200 GPasegment 2: bronze, Ø60 mm, 500 mm, E = 110 GPaP = 60 kN
σ2 = MPa
9.Column bucklingMedium
PL = 5 md = 80 mmcross-section

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

L = 5 mE = 70 GPa (aluminium)d = 80 mm
Pcr = kN
10.Column bucklingHard
PL = 4 md = 40 mmcross-section

A column of length L made of aluminium is fixed at the base and pinned at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 4 mE = 70 GPa (aluminium)d = 40 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 40 kN/mc = 240 N·s/mm = 150 kg

A 150 kg mass is supported by a spring with a stiffness of 40 kN/m and a viscous damper with a damping coefficient of 240 N·s/m. Find the damping ratio ζ.

m = 150 kgk = 40 kN/mc = 240 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 12k2​ = 12k3​ = 60m = 25 kg

A 25 kg mass hangs from spring k₃ = 60 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 = 12 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 = 25 kgk1 = 12 kN/mk2 = 12 kN/mk3 = 60 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: Ft = 4663 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·960/60 = 100.5 rad/s
T = P/ω = 15000/100.5 = 149.2 N·m

Pitch diameter

d = m·N = 4·16 = 64 mm

Tangential force

Ft = 2T/d = 2·149.2/0.064 = 4663 N

Answer

Ft = 4663 N
2.Gears & gear trains

Answer: nout = 234.4 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 = 1500·15/40 = 562.5 rpm = nC

Second stage

nout = 562.5·20/48 = 234.4 rpm

Answer

nout = 234.4 rpm

total ratio = 6.4 : 1

3.Torsion of shafts

Answer: φ = 4.029 °

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(40⁴ − 24⁴)/32 = 218755 mm⁴

Angle of twist

T = 400 N·m = 400000 N·mm
L = 1 m = 1000 mm
G = 26 GPa = 26000 MPa
φ = TL/(GJ) = 400000·1000/(26000·218755) = 0.07033 rad
φ = 0.07033·180/π = 4.029°

Answer

φ = 4.029°
4.Torsion of shafts

Answer: do = 12.3 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·3000/60 = 314.2 rad/s
T = P/ω = 5000/314.2 = 15.92 N·m

Outer diameter from the allowable stress

T = 15.92 N·m = 15915 N·mm
1 − k⁴ = 1 − 0.6⁴ = 0.8704
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·15915/(π·50·0.8704)) = 12.3 mm
di = 0.6·12.3 = 7.382 mm

Answer

do = 12.3 mm

A solid shaft would need d = 11.75 mm; the hollow one is a little larger but much lighter.

5.Mohr’s circle & stress transformation

Answer: θp = −47.86 °

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·−50, 20 − 30) = −95.71°

Angle on the element

θp = −47.86°

Answer

θp = −47.86°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: τθ = 76.29 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

τθ = −65·−0.866 + 40·0.5 = 76.29 MPa

Answer

τθ = 76.29 MPa
7.Axial stress & strain

Answer: P = 74.23 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 = 1257 mm², A₂ = 706.9 mm²

Flexibilities

L₁/(E₁A₁) = 400/(200000·1257) = 1.592 × 10⁻⁶ mm/N
L₂/(E₂A₂) = 400/(110000·706.9) = 5.144 × 10⁻⁶ mm/N

Load

P = 0.5/6.736 × 10⁻⁶ = 74229 N = 74.23 kN

Answer

P = 74.23 kN
8.Axial stress & strain

Answer: σ2 = 12.07 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 = 200000·706.9/300 = 471239 N/mm
k₂ = 110000·2827/500 = 622035 N/mm

Share of segment 2

F2 = 60000·622035/1.093 × 10⁶ = 34138 N

Stress

σ2 = 34138/2827 = 12.07 MPa (compression)

Answer

σ2 = 12.07 MPa
9.Column buckling

Answer: Pcr = 222.3 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·80⁴/64 = 2.011 × 10⁶ mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·2.011 × 10⁶/2500² = 222253 N = 222.3 kN

Answer

Pcr = 222.3 kN
10.Column buckling

Answer: σcr = 8.812 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 = 0.7·4000 = 2800 mm
KL/r = 2800/10 = 280

Critical stress

σcr = π²E/(KL/r)² = π²·70000/280² = 8.812 MPa

Answer

σcr = 8.812 MPa
11.Mechanical vibrations

Answer: ζ = 0.04899

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·√(40000·150) = 4899 N·s/m

Damping ratio

ζ = c/cc = 240/4899 = 0.04899

Answer

ζ = 0.04899

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

12.Mechanical vibrations

Answer: fn = 4.168 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 + 12 = 24 kN/m
keq = 24·60/(24 + 60) = 17.14 kN/m

Natural frequency

ωn = √(17143/25) = 26.19 rad/s
fn = 26.19/(2π) = 4.168 Hz

Answer

fn = 4.168 Hz

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