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​ = 25N2​ = 30

A 3 kW motor running at 1440 rpm drives a pinion with 25 teeth, which meshes with a gear with 30 teeth. The gear pair has an efficiency of 97%. Find the output torque T2 on the gear shaft.

P = 3 kWn1 = 1440 rpmN1 = 25N2 = 30η = 97%
T2 = N·m
2.Gears & gear trainsHard
A = 24B = 25C = 18D = 72

In a compound gear train, gear A (24 teeth) on the input shaft turning at 1450 rpm drives gear B (25 teeth). Gear C (18 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 = 1450 rpmA = 24B = 25C = 18D = 72
nout = rpm
3.Torsion of shaftsMedium
T = 500 N·md = 30 mmL = 1 mφ = ?

A solid brass 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 = 500 N·md = 30 mmL = 1 mG = 39 GPa
φ = °
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 30 kW at 1500 rpm without the shear stress exceeding 80 MPa. Find the smallest diameter d that works.

P = 30 kWN = 1500 rpmτallow = 80 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 60σy​ = 110τxy​ = 50MPa

A point has σₓ = 60 MPa, σᵧ = 110 MPa and τₓᵧ = 50 MPa (tension positive). Find the angle θs, between −90° and 90°, from the x-axis to the normal of the plane on which the shear stress has its maximum positive value +R (shear positive in the same sense as τₓᵧ).

σx = 60 MPaσy = 110 MPaτxy = 50 MPa
θs = °
6.Mohr’s circle & stress transformationHard
σx​τxy​surface of the shaft

A solid shaft of diameter 50 mm carries an axial compressive force of 100 kN together with a torque of 2000 N·m. At the surface of the shaft, find the largest principal stress σ1.

d = 50 mmF = −100 kNT = 2000 N·m
σ1 = MPa
7.Axial stress & strainMedium
P = ?12400 mm300 mmØ40Ø60δ = 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 brass (diameter 60 mm, length 300 mm, E = 100 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: brass, Ø60 mm, 300 mm, E = 100 GPaδ = 0.5 mm
P = kN
8.Axial stress & strainHard
60 kN12400 mm300 mmØ40Ø40σ2​ = ?

A steel segment (diameter 40 mm, length 400 mm, E = 200 GPa) and a segment made of aluminium (diameter 40 mm, length 300 mm, E = 70 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, Ø40 mm, 400 mm, E = 200 GPasegment 2: aluminium, Ø40 mm, 300 mm, E = 70 GPaP = 60 kN
σ2 = MPa
9.Column bucklingMedium
PL = 2 md = 20 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 = 2 mE = 70 GPa (aluminium)d = 20 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 50 mmcross-section

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

L = 2.5 mE = 70 GPa (aluminium)d = 50 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 100 kN/mζ = 0.6m = 40 kg

A 40 kg mass on a spring with a stiffness of 100 kN/m has a viscous damper giving a damping ratio of 0.6. Find the damped natural frequency fd of its free vibration in Hz.

m = 40 kgk = 100 kN/mζ = 0.6
fd = Hz
12.Mechanical vibrationsHard
k1​ = 50k2​ = 80k3​ = 100m = 40 kg

A 40 kg mass hangs from spring k₃ = 100 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 50 kN/m and k₂ = 80 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 = 40 kgk1 = 50 kN/mk2 = 80 kN/mk3 = 100 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: T2 = 23.16 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·1440/60 = 150.8 rad/s
T1 = P/ω₁ = 3000/150.8 = 19.89 N·m

Output torque

T2 = 19.89·30/25·0.97 = 23.16 N·m

Answer

T2 = 23.16 N·m
2.Gears & gear trains

Answer: nout = 348 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 = 1450·24/25 = 1392 rpm = nC

Second stage

nout = 1392·18/72 = 348 rpm

Answer

nout = 348 rpm

total ratio = 4.167 : 1

3.Torsion of shafts

Answer: φ = 9.237 °

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·30⁴/32 = 79522 mm⁴

Angle of twist

φ = TL/(GJ) = 500·1000·1000/(39000·79522) = 0.1612 rad
φ = 0.1612·180/π = 9.237°

Answer

φ = 9.237°
4.Torsion of shafts

Answer: d = 22.99 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 = 30000/157.1 = 191 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·190986/(π·80)) = 22.99 mm

Answer

d = 22.99 mm

In practice you would round up to the next standard size.

5.Mohr’s circle & stress transformation

Answer: θs = 13.28 °

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​

Angle on the circle

On Mohr’s circle the top point (+R) is 90° from the principal point σ₁; on the element that is 45°.

cos 2θs = 50/55.9 = 0.8944, sin 2θs = −(−25)/55.9 = 0.4472
2θs = atan2(25, 50) = 26.57°

Angle on the element

θs = 13.28°
check: θs − θp = 13.28 − 58.28 = −45°

Answer

θs = 13.28°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: σ1 = 59.91 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 = −100000/(π·50²/4) = −100000/1963 = −50.93 MPa
τ = 16T/(πd³) = 16·2000000/(π·50³) = 81.49 MPa
στxyCσ1​σ2​

Mohr’s circle

C = σ/2 = −25.46 MPa
R = √((−25.46)² + 81.49²) = 85.37 MPa
σ1 = C + R = 59.91 MPa
σ2 = C − R = −110.8 MPa

Answer

σ1 = 59.91 MPa
7.Axial stress & strain

Answer: P = 188.5 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 = 2827 mm²

Flexibilities

L₁/(E₁A₁) = 400/(200000·1257) = 1.592 × 10⁻⁶ mm/N
L₂/(E₂A₂) = 300/(100000·2827) = 1.061 × 10⁻⁶ mm/N

Load

P = 0.5/2.653 × 10⁻⁶ = 188496 N = 188.5 kN

Answer

P = 188.5 kN
8.Axial stress & strain

Answer: σ2 = 15.19 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 = 200000·1257/400 = 628319 N/mm
k₂ = 70000·1257/300 = 293215 N/mm

Share of segment 2

F2 = 60000·293215/921534 = 19091 N

Stress

σ2 = 19091/1257 = 15.19 MPa (compression)

Answer

σ2 = 15.19 MPa
9.Column buckling

Answer: Pcr = 5.426 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·20⁴/64 = 7854 mm⁴

Effective length

KL = 0.5·2000 = 1000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·7854/1000² = 5426 N = 5.426 kN

Answer

Pcr = 5.426 kN
10.Column buckling

Answer: σcr = 69.09 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·50⁴/64 = 306796 mm⁴

Radius of gyration and slenderness

A = 1963 mm²
r = √(I/A) = √(306796/1963) = 12.5 mm
KL = 0.5·2500 = 1250 mm
KL/r = 1250/12.5 = 100

Critical stress

σcr = π²E/(KL/r)² = π²·70000/100² = 69.09 MPa

Answer

σcr = 69.09 MPa
11.Mechanical vibrations

Answer: fd = 6.366 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 = √(100000/40) = 50 rad/s
fn = 50/(2π) = 7.958 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 7.958·√(1 − 0.6²) = 6.366 Hz

Answer

fd = 6.366 Hz
12.Mechanical vibrations

Answer: fn = 5.983 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 = 50 + 80 = 130 kN/m
keq = 130·100/(130 + 100) = 56.52 kN/m

Natural frequency

ωn = √(56522/40) = 37.59 rad/s
fn = 37.59/(2π) = 5.983 Hz

Answer

fn = 5.983 Hz

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