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
Nw​ = 36z = 3, 1440 rpm

A worm with 3 start(s) turns at 1440 rpm and drives a worm wheel with 36 teeth. Find the speed nw of the wheel.

z = 3Nw = 36n = 1440 rpm
nw = rpm
2.Gears & gear trainsHard
A = 18B = 36C = 24D = 40

In a compound gear train, gear A (18 teeth) on the input shaft turning at 960 rpm drives gear B (36 teeth). Gear C (24 teeth) is fixed to the same shaft as B and drives gear D (40 teeth) on the output shaft. Find the output speed nout.

nin = 960 rpmA = 18B = 36C = 24D = 40
nout = rpm
3.Torsion of shaftsMedium
T = 200 N·md = 25 mmL = 0.5 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 = 200 N·md = 25 mmL = 0.5 mG = 39 GPa
φ = °
4.Torsion of shaftsHard
d = 30 mmTB​ = 200 N·mTC​ = 250 N·mABC1 m2 m

A solid steel shaft of diameter 30 mm is fixed at A. A torque of 200 N·m acts at B, 1 m from A, and a torque of 250 N·m in the opposite direction acts at the free end C, a further 2 m along. Find the maximum shear stress τmax in the shaft.

d = 30 mmTB = 200 N·mTC = 250 N·mAB = 1 mBC = 2 m
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = 10σy​ = 50τxy​ = 40MPa

A point in a loaded part has σₓ = 10 MPa, σᵧ = 50 MPa and τₓᵧ = 40 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = 10 MPaσy = 50 MPaτxy = 40 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 70σy​ = −40τxy​ = 30MPa

A point in a loaded part has σₓ = 70 MPa, σᵧ = −40 MPa and τₓᵧ = 30 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 20° clockwise from the x-axis (positive in the same sense as τₓᵧ).

σx = 70 MPaσy = −40 MPaτxy = 30 MPaθ = -20°
τθ = MPa
7.Axial stress & strainMedium
100 kNØ30110 GPaØ100/70600 mmδ = ?

A steel rod (diameter 30 mm, E = 200 GPa) sits inside a tube made of bronze (outer diameter 100 mm, inner diameter 70 mm, E = 110 GPa). Both are 600 mm long and are compressed together between rigid plates by 100 kN. Find the shortening δ.

P = 100 kNrod: Ø30 mm, E = 200 GPatube: Ø100/Ø70 mm, E = 110 GPaL = 600 mm
δ = mm
8.Axial stress & strainHard
Ø 35 mmSteel1 mØ 20 mmBrass2 mP = 80 kN

The stepped bar is fixed at the wall and loaded at its free end. Find the total elongation δ.

P = 80 kNsegment 1: Ø35 mm, 1 m, steel (E = 200 GPa)segment 2: Ø20 mm, 2 m, brass (E = 100 GPa)
δ = mm
9.Column bucklingMedium
PL = 3 m50 × 60 mmcross-section

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

L = 3 mE = 200 GPa (steel)b × h = 50 × 60 mm
Pcr = kN
10.Column bucklingHard
PL = 2 md = 50 mmcross-section

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

L = 2 mE = 70 GPa (aluminium)d = 50 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 5 kN/mc = 70 N·s/mm = 10 kg

A 10 kg mass is supported by a spring with a stiffness of 5 kN/m and a viscous damper with a damping coefficient of 70 N·s/m. Find the damping ratio ζ.

m = 10 kgk = 5 kN/mc = 70 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 12k2​ = 30m = 10 kg

A 10 kg mass hangs from two springs connected end to end (in series): the upper spring has k₁ = 12 kN/m and the lower one k₂ = 30 kN/m. Find the equivalent stiffness keq of the spring system in kN/m.

m = 10 kgk1 = 12 kN/mk2 = 30 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: nw = 120 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.

Wheel speed

nw = n·z/Nw = 1440·3/36 = 120 rpm

Answer

nw = 120 rpm
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 = 960·18/36 = 480 rpm = nC

Second stage

nout = 480·24/40 = 288 rpm

Answer

nout = 288 rpm

total ratio = 3.333 : 1

3.Torsion of shafts

Answer: φ = 3.831 °

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·25⁴/32 = 38350 mm⁴

Angle of twist

φ = TL/(GJ) = 200·1000·500/(39000·38350) = 0.06686 rad
φ = 0.06686·180/π = 3.831°

Answer

φ = 3.831°
4.Torsion of shafts

Answer: τmax = 47.16 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.

Internal torques

Sense of TC taken as positive.

TBC = TC = 250 N·m
TAB = TC − TB = 250 − 200 = 50 N·m

Maximum shear stress

The segment with the largest internal torque has the largest stress (same diameter).

|T|max = 250 N·m
τmax = 16·250000/(π·30³) = 47.16 MPa

Answer

τmax = 47.16 MPa
5.Mohr’s circle & stress transformation

Answer: τmax = 44.72 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 = √(((10 − 50)/2)² + 40²) = 44.72 MPa

Answer

τmax = 44.72 MPa
6.Mohr’s circle & stress transformation

Answer: τθ = 58.33 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 = −55·−0.6428 + 30·0.766 = 58.33 MPa

Answer

τθ = 58.33 MPa
7.Axial stress & strain

Answer: δ = 0.1031 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·30²/4 = 706.9 mm²
At = π(100² − 70²)/4 = 4006 mm²

Combined axial stiffness

ΣEA = 200·10³·706.9 + 110·10³·4006 = 5.82 × 10⁸ N

Shortening

δ = 100000·600/5.82 × 10⁸ = 0.1031 mm

Answer

δ = 0.1031 mm
8.Axial stress & strain

Answer: δ = 5.509 mm

Axially loaded members: each prismatic segment obeys δ = PL/(AE). For members in series the elongations add.

Same force in both segments

The free end carries P, so every section of the bar carries the same axial force P. Only the areas and materials change.

A1 = π·35²/4 = 962.1 mm², A2 = π·20²/4 = 314.2 mm²
σ1 = 83.15 MPa
σ2 = 254.6 MPa

Add the segment elongations

δ1 = σ1L1/E1 = 83.15·1000/200000 = 0.4158 mm
δ2 = σ2L2/E2 = 254.6·2000/100000 = 5.093 mm
δ = δ1 + δ2 = 5.509 mm

Answer

δ = 5.509 mm
9.Column buckling

Answer: Pcr = 137.1 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 = 1·3000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·625000/3000² = 137078 N = 137.1 kN

Answer

Pcr = 137.1 kN
10.Column buckling

Answer: σcr = 6.747 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 = 2·2000 = 4000 mm
KL/r = 4000/12.5 = 320

Critical stress

σcr = π²E/(KL/r)² = π²·70000/320² = 6.747 MPa

Answer

σcr = 6.747 MPa
11.Mechanical vibrations

Answer: ζ = 0.1565

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·√(5000·10) = 447.2 N·s/m

Damping ratio

ζ = c/cc = 70/447.2 = 0.1565

Answer

ζ = 0.1565

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

12.Mechanical vibrations

Answer: keq = 8.571 kN/m

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 in series share the same force and add their deflections, so they combine as reciprocals: 1/k = 1/k1 + 1/k2.

1/keq = 1/12 + 1/30 → keq = 12·30/(12 + 30) = 8.571 kN/m

Answer

keq = 8.571 kN/m

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