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​ = 45z = 3, 1450 rpm

A worm with 3 start(s) turns at 1450 rpm and drives a worm wheel with 45 teeth. Find the speed nw of the wheel.

z = 3Nw = 45n = 1450 rpm
nw = rpm
2.Gears & gear trainsHard
d1​ = 150 mmd2​ = 500 mm1500 rpmC = 800 mmT1​ = 800 NT2​P = ?

An open belt connects a 150 mm driving pulley at 1500 rpm to a 500 mm pulley; the centres are 800 mm apart. The coefficient of friction is 0.25 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 = 150 mmn1 = 1500 rpmd2 = 500 mmC = 800 mmμ = 0.25T1 = 800 N
P = kW
3.Torsion of shaftsMedium
do​ = 40, di​ = 28 mmT = 400 N·mL = 1 m

A hollow aluminium shaft (outer diameter 40 mm, inner diameter 28 mm, length 1 m) is fixed at one end and twisted by a torque of 400 N·m at the other. Find the angle of twist φ in degrees.

T = 400 N·mdo = 40 mmdi = 28 mmL = 1 mG = 26 GPa
φ = °
4.Torsion of shaftsHard
Tdo​ = 50 mm, di​ = 25 mm

A hollow shaft transmits 75 kW at 3000 rpm. Find the maximum shear stress τmax in the shaft.

P = 75 kWN = 3000 rpmdo = 50 mmdi = 25 mm
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = −40σy​ = 120τxy​ = −30MPa

A point in a loaded part has σₓ = −40 MPa, σᵧ = 120 MPa and τₓᵧ = −30 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = −40 MPaσy = 120 MPaτxy = −30 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 150σy​ = −20τxy​ = −40MPa

A point in a loaded part has σₓ = 150 MPa, σᵧ = −20 MPa and τₓᵧ = −40 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 60° counter-clockwise from the x-axis.

σx = 150 MPaσy = −20 MPaτxy = −40 MPaθ = 60°
σθ = MPa
7.Axial stress & strainMedium
Ø 25 mmAluminium1 mP = 45 kN

Find the axial strain ε in the aluminium bar, in microstrain (µε = 10⁻⁶).

P = 45 kNd = 25 mmL = 1 mE = 70 GPa
ε = µε
8.Axial stress & strainHard
Ø 35 mmBrass1 mØ 20 mmAluminium1 mP = 60 kN

The stepped bar is fixed at the wall and loaded at its free end. Find the largest normal stress σmax in the bar.

P = 60 kNsegment 1: Ø35 mm, 1 m, brass (E = 100 GPa)segment 2: Ø20 mm, 1 m, aluminium (E = 70 GPa)
σmax = MPa
9.Column bucklingMedium
PL = 5 md = 40 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 = 5 mE = 200 GPa (steel)d = 40 mm
Pcr = kN
10.Column bucklingHard
PL = 1.5 md = 60 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 = 1.5 mE = 70 GPa (aluminium)d = 60 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 8 kN/mc = 50 N·s/mm = 8 kg

An 8 kg mass is supported by a spring with a stiffness of 8 kN/m and a viscous damper with a damping coefficient of 50 N·s/m. Find the damping ratio ζ.

m = 8 kgk = 8 kN/mc = 50 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 10k2​ = 80m = 40 kg

A 40 kg mass hangs from two springs connected end to end (in series): the upper spring has k₁ = 10 kN/m and the lower one k₂ = 80 kN/m. Find the equivalent stiffness keq of the spring system in kN/m.

m = 40 kgk1 = 10 kN/mk2 = 80 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: nw = 96.67 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 = 1450·3/45 = 96.67 rpm

Answer

nw = 96.67 rpm
2.Gears & gear trains

Answer: P = 4.627 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 = 2.701 rad

Slack-side tension

eμθ = e0.6751 = 1.964, T₂ = 800/1.964 = 407.3 N

Power

P = (800 − 407.3)·11.78 = 4.627 kW

Answer

P = 4.627 kW
3.Torsion of shafts

Answer: φ = 4.615 °

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 − 28⁴)/32 = 190984 mm⁴

Angle of twist

T = 400 N·m = 400000 N·mm
L = 1 m = 1000 mm
G = 26 GPa = 26000 MPa
φ = TL/(GJ) = 400000·1000/(26000·190984) = 0.08055 rad
φ = 0.08055·180/π = 4.615°

Answer

φ = 4.615°
4.Torsion of shafts

Answer: τmax = 10.38 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·3000/60 = 314.2 rad/s
T = P/ω = 75000/314.2 = 238.7 N·m

Polar second moment of area

J = π(50⁴ − 25⁴)/32 = 575243 mm⁴

Maximum shear stress

τmax = T·(do/2)/J = 238732·25/575243 = 10.38 MPa

Answer

τmax = 10.38 MPa
5.Mohr’s circle & stress transformation

Answer: τmax = 85.44 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 = √(((−40 − 120)/2)² + −30²) = 85.44 MPa

Answer

τmax = 85.44 MPa
6.Mohr’s circle & stress transformation

Answer: σθ = −12.14 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 = 65 + 85·−0.5 + −40·0.866 = −12.14 MPa

Answer

σθ = −12.14 MPa
7.Axial stress & strain

Answer: ε = 1310 µε

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·25²/4 = 490.9 mm²
σ = P/A = 45·1000/490.9 = 91.67 MPa

Strain (Hooke’s law)

E for aluminium = 70 GPa = 70000 MPa.

ε = σ/E = 91.67/70000 = 0.00131 = 1310 µε

Answer

ε = 1310 µε
8.Axial stress & strain

Answer: σmax = 191 MPa

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 = 62.36 MPa
σ2 = 191 MPa

Largest stress

The thinner segment has the smaller area, so it carries the larger stress.

σmax = 191 MPa

Answer

σmax = 191 MPa
9.Column buckling

Answer: Pcr = 9.922 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·40⁴/64 = 125664 mm⁴

Effective length

KL = 1·5000 = 5000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·125664/5000² = 9922 N = 9.922 kN

Answer

Pcr = 9.922 kN
10.Column buckling

Answer: σcr = 17.27 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·60⁴/64 = 636173 mm⁴

Radius of gyration and slenderness

A = 2827 mm²
r = √(I/A) = √(636173/2827) = 15 mm
KL = 2·1500 = 3000 mm
KL/r = 3000/15 = 200

Critical stress

σcr = π²E/(KL/r)² = π²·70000/200² = 17.27 MPa

Answer

σcr = 17.27 MPa
11.Mechanical vibrations

Answer: ζ = 0.09882

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·√(8000·8) = 506 N·s/m

Damping ratio

ζ = c/cc = 50/506 = 0.09882

Answer

ζ = 0.09882

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

12.Mechanical vibrations

Answer: keq = 8.889 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 = 1/10 + 1/80 → keq = 10·80/(10 + 80) = 8.889 kN/m

Answer

keq = 8.889 kN/m

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