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​ = 50N2​ = 60

A 5.5 kW motor running at 960 rpm drives a pinion with 50 teeth, which meshes with a gear with 60 teeth. The gear pair has an efficiency of 95%. Find the output torque T2 on the gear shaft.

P = 5.5 kWn1 = 960 rpmN1 = 50N2 = 60η = 95%
T2 = N·m
2.Gears & gear trainsHard
A = 30B = 40C = 16D = 60

In a compound gear train, gear A (30 teeth) on the input shaft turning at 1440 rpm drives gear B (40 teeth). Gear C (16 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 = 30B = 40C = 16D = 60
nout = rpm
3.Torsion of shaftsMedium
T = 250 N·md = 40 mmL = 2.5 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 = 40 mmL = 2.5 mG = 80 GPa
φ = °
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 75 kW at 500 rpm without the shear stress exceeding 75 MPa. Find the smallest diameter d that works.

P = 75 kWN = 500 rpmτallow = 75 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σy​ = 40τxy​ = 10MPa

A point has σₓ = 0 MPa, σᵧ = 40 MPa and τₓᵧ = 10 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 = 0 MPaσy = 40 MPaτxy = 10 MPa
θs = °
6.Mohr’s circle & stress transformationHard
55°D = 500 mm, t = 6 mm, p = 3 MPap

A thin-walled cylindrical tank of inner diameter 500 mm and wall thickness 6 mm holds gas at a gauge pressure of 3 MPa. It is made from plate welded along a helical seam at 55° to the axis of the cylinder. Find the normal stress σn acting across the weld seam.

D = 500 mmt = 6 mmp = 3 MPaα = 55°
σn = MPa
7.Axial stress & strainMedium
100 kNØ40120 GPaØ120/70300 mmδ = ?

A steel rod (diameter 40 mm, E = 200 GPa) sits inside a tube made of copper (outer diameter 120 mm, inner diameter 70 mm, E = 120 GPa). Both are 300 mm long and are compressed together between rigid plates by 100 kN. Find the shortening δ.

P = 100 kNrod: Ø40 mm, E = 200 GPatube: Ø120/Ø70 mm, E = 120 GPaL = 300 mm
δ = mm
8.Axial stress & strainHard
P = ?Ø30100 GPaØ100/70600 mm

A steel rod (diameter 30 mm, E = 200 GPa, allowable stress 200 MPa) sits inside a tube made of brass (outer diameter 100 mm, inner diameter 70 mm, E = 100 GPa, allowable stress 70 MPa). They are compressed together between rigid plates. Find the largest load Pmax.

rod: Ø30 mm, E = 200 GPa, σallow = 200 MPatube: Ø100/Ø70 mm, E = 100 GPa, σallow = 70 MPa
Pmax = kN
9.Column bucklingMedium
PL = 4 m50 × 60 mmcross-section

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

L = 4 mE = 70 GPa (aluminium)b × h = 50 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 15 kNL = 2 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and free at the top. It must carry 15 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 15 kNn = 2.5L = 2 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
tx50 mm3 cycles11 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 50 mm is followed 3 cycles later by a peak of 11 mm. Find the damping ratio ζ.

x0 = 50 mmx3 = 11 mmn = 3
ζ =
12.Mechanical vibrationsHard
k1​ = 10k2​ = 40k3​ = 60m = 10 kg

A 10 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 = 10 kN/m and k₂ = 40 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 = 10 kgk1 = 10 kN/mk2 = 40 kN/mk3 = 60 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: T2 = 62.37 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·960/60 = 100.5 rad/s
T1 = P/ω₁ = 5500/100.5 = 54.71 N·m

Output torque

T2 = 54.71·60/50·0.95 = 62.37 N·m

Answer

T2 = 62.37 N·m
2.Gears & gear trains

Answer: nout = 288 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 = 1440·30/40 = 1080 rpm = nC

Second stage

nout = 1080·16/60 = 288 rpm

Answer

nout = 288 rpm

total ratio = 5 : 1

3.Torsion of shafts

Answer: φ = 1.781 °

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) = 250·1000·2500/(80000·251327) = 0.03108 rad
φ = 0.03108·180/π = 1.781°

Answer

φ = 1.781°
4.Torsion of shafts

Answer: d = 45.99 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·500/60 = 52.36 rad/s
T = P/ω = 75000/52.36 = 1432 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·1.432 × 10⁶/(π·75)) = 45.99 mm

Answer

d = 45.99 mm

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

5.Mohr’s circle & stress transformation

Answer: θs = 31.72 °

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 = 10/22.36 = 0.4472, sin 2θs = −(−20)/22.36 = 0.8944
2θs = atan2(20, 10) = 63.43°

Angle on the element

θs = 31.72°
check: θs − θp = 31.72 − 76.72 = −45°

Answer

θs = 31.72°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: σn = 83.06 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. Thin-walled cylinder: hoop stress σh = pr/t and axial stress σa = pr/(2t); these are the principal stresses in the wall.

Wall stresses

r = 500/2 = 250 mm
σh = pr/t = 3·250/6 = 125 MPa
σa = pr/(2t) = 62.5 MPa

Transform to the seam

Take x along the axis (σa) and y around the hoop (σh). The seam’s normal makes 90° − α with the axis.

σn = 62.5·sin²55° + 125·cos²55° = 83.06 MPa

Answer

σn = 83.06 MPa
7.Axial stress & strain

Answer: δ = 0.02616 mm

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·40²/4 = 1257 mm²
At = π(120² − 70²)/4 = 7461 mm²

Combined axial stiffness

ΣEA = 200·10³·1257 + 120·10³·7461 = 1.147 × 10⁹ N

Shortening

δ = 100000·300/1.147 × 10⁹ = 0.02616 mm

Answer

δ = 0.02616 mm
8.Axial stress & strain

Answer: Pmax = 379.3 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·30²/4 = 706.9 mm²
At = π(100² − 70²)/4 = 4006 mm²

Combined axial stiffness

ΣEA = 200·10³·706.9 + 100·10³·4006 = 5.419 × 10⁸ N

Governing strain

ε = min(0.001, 0.0007) = 0.0007 (brass)

Largest load

Pmax = 0.0007·5.419 × 10⁸ = 379347 N = 379.3 kN

Answer

Pmax = 379.3 kN
9.Column buckling

Answer: Pcr = 26.99 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 = 60·50³/12 = 625000 mm⁴

Effective length

KL = 1·4000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·625000/4000² = 26987 N = 26.99 kN

Answer

Pcr = 26.99 kN
10.Column buckling

Answer: d = 49.88 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 = 2.5·15000 = 37500 N
KL = 2·2000 = 4000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·37500·4000²/(π³·200000))^(1/4) = 49.88 mm

Answer

d = 49.88 mm

Check: the slenderness KL/r is 320.7, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.08007

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.

Logarithmic decrement

δ = (1/3)·ln(50/11) = 0.5047

Damping ratio

ζ = δ/√(4π² + δ²) = 0.5047/√(39.48 + 0.2547) = 0.08007

Answer

ζ = 0.08007
12.Mechanical vibrations

Answer: fn = 8.312 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 = 10 + 40 = 50 kN/m
keq = 50·60/(50 + 60) = 27.27 kN/m

Natural frequency

ωn = √(27273/10) = 52.22 rad/s
fn = 52.22/(2π) = 8.312 Hz

Answer

fn = 8.312 Hz

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