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
d1​ = 100 mmd2​ = 200 mm1450 rpmn2​ = ?

A 100 mm pulley at 1450 rpm drives a 200 mm pulley by a belt with 1.5 % slip. Find the speed n2 of the driven pulley.

n1 = 1450 rpmd1 = 100 mmd2 = 200 mms = 1.5 %
n2 = rpm
2.Gears & gear trainsHard
d1​ = 80 mmd2​ = 450 mm1450 rpmC = 500 mmT1​ = 800 NT2​P = ?

An open belt connects an 80 mm driving pulley at 1450 rpm to a 450 mm pulley; the centres are 500 mm apart. The coefficient of friction is 0.3 and the tight-side tension may not exceed 800 N. Find the largest power P the belt can transmit without slipping, in kW (ignore centrifugal effects).

d1 = 80 mmn1 = 1450 rpmd2 = 450 mmC = 500 mmμ = 0.3T1 = 800 N
P = kW
3.Torsion of shaftsMedium
T = 500 N·md = 40 mmL = 3 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 = 500 N·md = 40 mmL = 3 mG = 80 GPa
φ = °
4.Torsion of shaftsHard
Tdo​ = 40 mm, di​ = 28 mm

A hollow shaft transmits 15 kW at 1800 rpm. Find the maximum shear stress τmax in the shaft.

P = 15 kWN = 1800 rpmdo = 40 mmdi = 28 mm
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = −80σy​ = 70τxy​ = −20MPa

A point has σₓ = −80 MPa, σᵧ = 70 MPa and τₓᵧ = −20 MPa (tension positive). The element is rotated 25° counter-clockwise. Find the normal stress σy′ on the faces of the rotated element that are perpendicular to the rotated y′-axis.

σx = −80 MPaσy = 70 MPaτxy = −20 MPaθ = 25°
σy′ = MPa
6.Mohr’s circle & stress transformationHard
σx​ = −60σy​ = 0τxy​ = −10MPa

A point in a loaded part has σₓ = −60 MPa, σᵧ = 0 MPa and τₓᵧ = −10 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 40° counter-clockwise from the x-axis (positive in the same sense as τₓᵧ).

σx = −60 MPaσy = 0 MPaτxy = −10 MPaθ = 40°
τθ = MPa
7.Axial stress & strainMedium
Ø 16 mmCopper2.5 mP = 55 kN

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

P = 55 kNd = 16 mmL = 2.5 mE = 117 GPa
δ = mm
8.Axial stress & strainHard
P = ?Ø20100 GPaØ80/50500 mm

A steel rod (diameter 20 mm, E = 200 GPa, allowable stress 160 MPa) sits inside a tube made of brass (outer diameter 80 mm, inner diameter 50 mm, E = 100 GPa, allowable stress 80 MPa). They are compressed together between rigid plates. Find the largest load Pmax.

rod: Ø20 mm, E = 200 GPa, σallow = 160 MPatube: Ø80/Ø50 mm, E = 100 GPa, σallow = 80 MPa
Pmax = kN
9.Column bucklingMedium
PL = 5 m25 × 50 mmcross-section

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

L = 5 mE = 200 GPa (steel)b × h = 25 × 50 mm
Pcr = kN
10.Column bucklingHard
PL = 1.5 md = 30 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 = 1.5 mE = 70 GPa (aluminium)d = 30 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 80 kN/mζ = 0.4m = 80 kg

An 80 kg mass on a spring with a stiffness of 80 kN/m has a viscous damper giving a damping ratio of 0.4. Find the damped natural frequency fd of its free vibration in Hz.

m = 80 kgk = 80 kN/mζ = 0.4
fd = Hz
12.Mechanical vibrationsHard
k1​ = 60k2​ = 20m = 25 kg

A 25 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 60 kN/m and k₂ = 20 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 = 25 kgk1 = 60 kN/mk2 = 20 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: n2 = 714.1 rpm

Belt drives: without slip, both pulleys have the same rim speed v = π·d·n/60, so n₁·d₁ = n₂·d₂ and the speed ratio is d₂/d₁. Slip s makes the driven pulley a little slower: n₂ = n₁·(d₁/d₂)·(1 − s). The power transmitted is P = (T₁ − T₂)·v, with T₁ the tension on the tight side and T₂ on the slack side. Friction limits the ratio of the tensions: T₁/T₂ = eμθ, where θ is the angle of wrap in radians on the smaller pulley; for an open belt θ = π − 2·asin((d₂ − d₁)/(2C)) with centre distance C.

Speed without slip

1450·100/200 = 725 rpm

With slip

n2 = 725·0.985 = 714.1 rpm

Answer

n2 = 714.1 rpm
2.Gears & gear trains

Answer: P = 2.482 kW

Belt drives: without slip, both pulleys have the same rim speed v = π·d·n/60, so n₁·d₁ = n₂·d₂ and the speed ratio is d₂/d₁. Slip s makes the driven pulley a little slower: n₂ = n₁·(d₁/d₂)·(1 − s). The power transmitted is P = (T₁ − T₂)·v, with T₁ the tension on the tight side and T₂ on the slack side. Friction limits the ratio of the tensions: T₁/T₂ = eμθ, where θ is the angle of wrap in radians on the smaller pulley; for an open belt θ = π − 2·asin((d₂ − d₁)/(2C)) with centre distance C.

Angle of wrap

θ = 2.384 rad

Slack-side tension

eμθ = e0.7151 = 2.044, T₂ = 800/2.044 = 391.3 N

Power

P = (800 − 391.3)·6.074 = 2.482 kW

Answer

P = 2.482 kW
3.Torsion of shafts

Answer: φ = 4.274 °

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·40⁴/32 = 251327 mm⁴

Angle of twist

φ = TL/(GJ) = 500·1000·3000/(80000·251327) = 0.0746 rad
φ = 0.0746·180/π = 4.274°

Answer

φ = 4.274°
4.Torsion of shafts

Answer: τmax = 8.333 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.

Torque

ω = 2πN/60 = 2π·1800/60 = 188.5 rad/s
T = P/ω = 15000/188.5 = 79.58 N·m

Polar second moment of area

J = π(40⁴ − 28⁴)/32 = 190984 mm⁴

Maximum shear stress

τmax = T·(do/2)/J = 79577·20/190984 = 8.333 MPa

Answer

τmax = 8.333 MPa
5.Mohr’s circle & stress transformation

Answer: σy′ = 58.53 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 for the y′ face

σy′ = −5 − (−75)·0.6428 − (−20)·0.766 = 58.53 MPa

Check

The sum of the normal stresses does not change with rotation.

σx′ = −68.53 MPa, σx′ + σy′ = −10 = σx + σy

Answer

σy′ = 58.53 MPa
6.Mohr’s circle & stress transformation

Answer: τθ = 27.81 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 = −−30·0.9848 + −10·0.1736 = 27.81 MPa

Answer

τθ = 27.81 MPa
7.Axial stress & strain

Answer: δ = 5.845 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·16²/4 = 201.1 mm²
σ = P/A = 55·1000/201.1 = 273.5 MPa

Strain (Hooke’s law)

E for copper = 117 GPa = 117000 MPa.

ε = σ/E = 273.5/117000 = 0.002338 = 2338 µε

Elongation

δ = ε·L = 0.002338·2500 mm = 5.845 mm

Answer

δ = 5.845 mm
8.Axial stress & strain

Answer: Pmax = 295.3 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(80² − 50²)/4 = 3063 mm²

Combined axial stiffness

ΣEA = 200·10³·314.2 + 100·10³·3063 = 3.691 × 10⁸ N

Governing strain

ε = min(0.0008, 0.0008) = 0.0008 (brass)

Largest load

Pmax = 0.0008·3.691 × 10⁸ = 295310 N = 295.3 kN

Answer

Pmax = 295.3 kN
9.Column buckling

Answer: Pcr = 20.56 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 = 50·25³/12 = 65104 mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·65104/2500² = 20562 N = 20.56 kN

Answer

Pcr = 20.56 kN
10.Column buckling

Answer: σcr = 35.25 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·30⁴/64 = 39761 mm⁴

Radius of gyration and slenderness

A = 706.9 mm²
r = √(I/A) = √(39761/706.9) = 7.5 mm
KL = 0.7·1500 = 1050 mm
KL/r = 1050/7.5 = 140

Critical stress

σcr = π²E/(KL/r)² = π²·70000/140² = 35.25 MPa

Answer

σcr = 35.25 MPa
11.Mechanical vibrations

Answer: fd = 4.613 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 = √(80000/80) = 31.62 rad/s
fn = 31.62/(2π) = 5.033 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 5.033·√(1 − 0.4²) = 4.613 Hz

Answer

fd = 4.613 Hz
12.Mechanical vibrations

Answer: fn = 9.003 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 = 60 + 20 = 80 kN/m

Natural frequency

ωn = √(80000/25) = 56.57 rad/s
fn = 56.57/(2π) = 9.003 Hz

Answer

fn = 9.003 Hz

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