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​ = 80 mmd2​ = 500 mm1450 rpmT1​ = 400 NT2​ = 200 NP = ?

A belt runs on an 80 mm driving pulley at 1450 rpm. The tension is 400 N on the tight side and 200 N on the slack side. Find the power P transmitted, in kW.

d1 = 80 mmn1 = 1450 rpmT1 = 400 NT2 = 200 N
P = kW
2.Gears & gear trainsHard
A = 32B = 80C = 40D = ?

In a compound gear train, gear A (32 teeth) on the input shaft turns at 960 rpm and drives gear B (80 teeth). Gear C (40 teeth) is fixed to the same shaft as B and drives gear D on the output shaft. The output must turn at 256 rpm. How many teeth ND must gear D have?

nin = 960 rpmA = 32B = 80C = 40nout = 256 rpm
ND =
3.Torsion of shaftsMedium
d = 15 mmT = 30 N·m200 mmφ = 2.66°

In a torsion test, a solid specimen of diameter 15 mm is twisted by a torque of 30 N·m. The two ends of a gauge length of 200 mm rotate 2.66° relative to each other (the material is still elastic). Find the shear modulus G of the material.

T = 30 N·md = 15 mmL = 200 mmφ = 2.66°
G = GPa
4.Torsion of shaftsHard
d = ?75 kW, 1500 rpm

A solid brass shaft transmits 75 kW at 1500 rpm. The shear stress must not exceed 60 MPa and the twist must not exceed 0.5° per m of length. Find the smallest diameter d that satisfies both limits.

P = 75 kWN = 1500 rpmτallow = 60 MPaθallow = 0.5°/mG = 39 GPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 140σy​ = −60τxy​ = 50MPa

A point in a loaded part has σₓ = 140 MPa, σᵧ = −60 MPa and τₓᵧ = 50 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = 140 MPaσy = −60 MPaτxy = 50 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 10σy​ = −80τxy​ = 10MPa

A point in a loaded part has σₓ = 10 MPa, σᵧ = −80 MPa and τₓᵧ = 10 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 20° counter-clockwise from the x-axis.

σx = 10 MPaσy = −80 MPaτxy = 10 MPaθ = 20°
σθ = MPa
7.Axial stress & strainMedium
P = ?12600 mm400 mmØ40Ø50δ = 0.2 mm

A bar is made of a steel segment (diameter 40 mm, length 600 mm, E = 200 GPa) joined end to end with a segment made of copper (diameter 50 mm, length 400 mm, E = 120 GPa). It is fixed at one end and pulled at the other. Find the axial load P that stretches it by 0.2 mm in total.

segment 1: steel, Ø40 mm, 600 mm, E = 200 GPasegment 2: copper, Ø50 mm, 400 mm, E = 120 GPaδ = 0.2 mm
P = kN
8.Axial stress & strainHard
40 kN12600 mm200 mmØ30Ø30σ2​ = ?

A steel segment (diameter 30 mm, length 600 mm, E = 200 GPa) and a segment made of copper (diameter 30 mm, length 200 mm, E = 120 GPa) are joined end to end and fixed between two rigid walls. An axial load of 40 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø30 mm, 600 mm, E = 200 GPasegment 2: copper, Ø30 mm, 200 mm, E = 120 GPaP = 40 kN
σ2 = MPa
9.Column bucklingMedium
PL = 4 m25 × 40 mmcross-section

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

L = 4 mE = 200 GPa (steel)b × h = 25 × 40 mm
Pcr = kN
10.Column bucklingHard
PL = 6 md = 30 mmcross-section

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

L = 6 mE = 200 GPa (steel)d = 30 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 50 kN/mc = 160 N·s/mm = 20 kg

A 20 kg mass is supported by a spring with a stiffness of 50 kN/m and a viscous damper with a damping coefficient of 160 N·s/m. Find the damping ratio ζ.

m = 20 kgk = 50 kN/mc = 160 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 25k2​ = 30k3​ = 10m = 25 kg

A 25 kg mass hangs from spring k₃ = 10 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 25 kN/m and k₂ = 30 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 = 25 kN/mk2 = 30 kN/mk3 = 10 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: P = 1.215 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.

Belt speed

v = 6.074 m/s

Power

P = (400 − 200)·6.074 = 1215 W = 1.215 kW

Answer

P = 1.215 kW
2.Gears & gear trains

Answer: ND = 60

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.

Intermediate shaft speed

nB = nC = 960·32/80 = 384 rpm

Teeth on gear D

ND = C·nC/nout = 40·384/256 = 60

Answer

ND = 60
3.Torsion of shafts

Answer: G = 26 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·15⁴/32 = 4970 mm⁴
φ = 2.66·π/180 = 0.04643 rad

Shear modulus

T = 30 N·m = 30000 N·mm
G = TL/(Jφ) = 30000·200/(4970·0.04643) = 26003 MPa
G = 26 GPa

Answer

G = 26 GPa

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

4.Torsion of shafts

Answer: d = 61.48 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

Diameter for strength

T = 477.5 N·m = 477465 N·mm
dτ = ∛(16·477465/(π·60)) = 34.35 mm

Diameter for stiffness

θ = 0.5·π/180/1000 = 8.727 × 10⁻⁶ rad/mm
G = 39 GPa = 39000 MPa
dφ = (32·477465/(π·39000·8.727 × 10⁻⁶))1/4 = 61.48 mm

Governing diameter

Both limits must hold, so the larger diameter governs.

d = max(34.35, 61.48) = 61.48 mm

Answer

d = 61.48 mm

Here stiffness governs.

5.Mohr’s circle & stress transformation

Answer: τmax = 111.8 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 = √(((140 − −60)/2)² + 50²) = 111.8 MPa

Answer

τmax = 111.8 MPa
6.Mohr’s circle & stress transformation

Answer: σθ = 5.9 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 = −35 + 45·0.766 + 10·0.6428 = 5.9 MPa

Answer

σθ = 5.9 MPa
7.Axial stress & strain

Answer: P = 48.96 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 = 1963 mm²

Flexibilities

L₁/(E₁A₁) = 600/(200000·1257) = 2.387 × 10⁻⁶ mm/N
L₂/(E₂A₂) = 400/(120000·1963) = 1.698 × 10⁻⁶ mm/N

Load

P = 0.2/4.085 × 10⁻⁶ = 48960 N = 48.96 kN

Answer

P = 48.96 kN
8.Axial stress & strain

Answer: σ2 = 36.38 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 = 200000·706.9/600 = 235619 N/mm
k₂ = 120000·706.9/200 = 424115 N/mm

Share of segment 2

F2 = 40000·424115/659734 = 25714 N

Stress

σ2 = 25714/706.9 = 36.38 MPa (compression)

Answer

σ2 = 36.38 MPa
9.Column buckling

Answer: Pcr = 13.11 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 = 40·25³/12 = 52083 mm⁴

Effective length

KL = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·52083/2800² = 13113 N = 13.11 kN

Answer

Pcr = 13.11 kN
10.Column buckling

Answer: σcr = 6.294 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 = 0.7·6000 = 4200 mm
KL/r = 4200/7.5 = 560

Critical stress

σcr = π²E/(KL/r)² = π²·200000/560² = 6.294 MPa

Answer

σcr = 6.294 MPa
11.Mechanical vibrations

Answer: ζ = 0.08

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·√(50000·20) = 2000 N·s/m

Damping ratio

ζ = c/cc = 160/2000 = 0.08

Answer

ζ = 0.08

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

12.Mechanical vibrations

Answer: fn = 2.928 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 = 25 + 30 = 55 kN/m
keq = 55·10/(55 + 10) = 8.462 kN/m

Natural frequency

ωn = √(8462/25) = 18.4 rad/s
fn = 18.4/(2π) = 2.928 Hz

Answer

fn = 2.928 Hz

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