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​ = 15N2​ = 50

A 15 kW motor running at 1440 rpm drives a pinion with 15 teeth, which meshes with a gear with 50 teeth. The gear pair has an efficiency of 96%. Find the torque T1 on the motor shaft.

P = 15 kWn1 = 1440 rpmN1 = 15N2 = 50η = 96%
T1 = N·m
2.Gears & gear trainsHard
A = 36B = 45C = 45D = 48

In a compound gear train, gear A (36 teeth) on the input shaft turning at 2900 rpm drives gear B (45 teeth). Gear C (45 teeth) is fixed to the same shaft as B and drives gear D (48 teeth) on the output shaft. Find the output speed nout.

nin = 2900 rpmA = 36B = 45C = 45D = 48
nout = rpm
3.Torsion of shaftsMedium
T = 400 N·md = 50 mmL = 1.5 mφ = ?

A solid aluminium 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 = 400 N·md = 50 mmL = 1.5 mG = 26 GPa
φ = °
4.Torsion of shaftsHard
do​ = ?50 kW, 1500 rpm

A hollow shaft must transmit 50 kW at 1500 rpm. Its inner diameter is to be 0.7 times its outer diameter, and the shear stress must not exceed 60 MPa. Find the smallest outer diameter do.

P = 50 kWN = 1500 rpmdi/do = 0.7τallow = 60 MPa
do = mm
5.Mohr’s circle & stress transformationMedium
σx​ = −10σy​ = 30τxy​ = −50MPa

A point has σₓ = −10 MPa, σᵧ = 30 MPa and τₓᵧ = −50 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 = −10 MPaσy = 30 MPaτxy = −50 MPa
θs = °
6.Mohr’s circle & stress transformationHard
σx​ = 50σy​ = 90τxy​ = 60MPa

A point in a thin plate is in plane stress: σₓ = 50 MPa, σᵧ = 90 MPa and τₓᵧ = 60 MPa (σz = 0). Find the von Mises equivalent stress σvM.

σx = 50 MPaσy = 90 MPaτxy = 60 MPa
σvM = MPa
7.Axial stress & strainMedium
Ø 25 mmAluminium1.5 mP = 105 kN

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

P = 105 kNd = 25 mmL = 1.5 mE = 70 GPa
ε = µε
8.Axial stress & strainHard
Ø 30 mmSteel2 mØ 12 mmCopper0.5 mP = 100 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 = 100 kNsegment 1: Ø30 mm, 2 m, steel (E = 200 GPa)segment 2: Ø12 mm, 0.5 m, copper (E = 117 GPa)
σmax = MPa
9.Column bucklingMedium
PL = 5 m30 × 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 = 5 mE = 200 GPa (steel)b × h = 30 × 40 mm
Pcr = kN
10.Column bucklingHard
P = 15 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and pinned 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 = 4 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
k = 50 kN/mc = 50 N·s/mm = 5 kg

A 5 kg mass is supported by a spring with a stiffness of 50 kN/m and a viscous damper with a damping coefficient of 50 N·s/m. Find the damping ratio ζ.

m = 5 kgk = 50 kN/mc = 50 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 15k2​ = 5m = 40 kg

A 40 kg mass hangs from two springs connected end to end (in series): the upper spring has k₁ = 15 kN/m and the lower one k₂ = 5 kN/m. Ignore damping and the masses of the springs. Find the natural frequency fn of vertical vibration in Hz.

m = 40 kgk1 = 15 kN/mk2 = 5 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: T1 = 99.47 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·1440/60 = 150.8 rad/s
T1 = P/ω₁ = 15000/150.8 = 99.47 N·m

Answer

T1 = 99.47 N·m
2.Gears & gear trains

Answer: nout = 2175 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 = 2900·36/45 = 2320 rpm = nC

Second stage

nout = 2320·45/48 = 2175 rpm

Answer

nout = 2175 rpm

total ratio = 1.333 : 1

3.Torsion of shafts

Answer: φ = 2.155 °

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·50⁴/32 = 613592 mm⁴

Angle of twist

φ = TL/(GJ) = 400·1000·1500/(26000·613592) = 0.03761 rad
φ = 0.03761·180/π = 2.155°

Answer

φ = 2.155°
4.Torsion of shafts

Answer: do = 32.88 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 = 50000/157.1 = 318.3 N·m

Outer diameter from the allowable stress

T = 318.3 N·m = 318310 N·mm
1 − k⁴ = 1 − 0.7⁴ = 0.7599
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·318310/(π·60·0.7599)) = 32.88 mm
di = 0.7·32.88 = 23.02 mm

Answer

do = 32.88 mm

A solid shaft would need d = 30.01 mm; the hollow one is a little larger but much lighter.

5.Mohr’s circle & stress transformation

Answer: θs = 79.1 °

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 = −50/53.85 = −0.9285, sin 2θs = −(−20)/53.85 = 0.3714
2θs = atan2(20, −50) = 158.2°

Angle on the element

θs = 79.1°
check: θs − θp = 79.1 − (−55.9) = 135°

Answer

θs = 79.1°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: σvM = 130 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. Yield criteria: von Mises predicts yield when σvM = √(σ₁² − σ₁σ₂ + σ₂²) reaches σY; Tresca when the absolute maximum shear stress reaches σY/2.

στxyCσ1​σ2​

Principal stresses

C = 70 MPa, R = 63.25 MPa
σ1 = 133.2 MPa, σ2 = 6.754 MPa, σ3 = 0

Von Mises

σvM = √(133.2² − 133.2·6.754 + 6.754²) = 130 MPa

Answer

σvM = 130 MPa
7.Axial stress & strain

Answer: ε = 3056 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 = 105·1000/490.9 = 213.9 MPa

Strain (Hooke’s law)

E for aluminium = 70 GPa = 70000 MPa.

ε = σ/E = 213.9/70000 = 0.003056 = 3056 µε

Answer

ε = 3056 µε
8.Axial stress & strain

Answer: σmax = 884.2 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·30²/4 = 706.9 mm², A2 = π·12²/4 = 113.1 mm²
σ1 = 141.5 MPa
σ2 = 884.2 MPa

Largest stress

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

σmax = 884.2 MPa

Answer

σmax = 884.2 MPa
9.Column buckling

Answer: Pcr = 14.5 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 = 40·30³/12 = 90000 mm⁴

Effective length

KL = 0.7·5000 = 3500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·90000/3500² = 14502 N = 14.5 kN

Answer

Pcr = 14.5 kN
10.Column buckling

Answer: d = 41.74 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 = 0.7·4000 = 2800 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·37500·2800²/(π³·200000))^(1/4) = 41.74 mm

Answer

d = 41.74 mm

Check: the slenderness KL/r is 268.4, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.05

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·√(50000·5) = 1000 N·s/m

Damping ratio

ζ = c/cc = 50/1000 = 0.05

Answer

ζ = 0.05

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

12.Mechanical vibrations

Answer: fn = 1.541 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 in series share the same force and add their deflections, so they combine as reciprocals: 1/k = 1/k1 + 1/k2.

1/keq = 1/15 + 1/5 → keq = 15·5/(15 + 5) = 3.75 kN/m

Natural frequency

ωn = √(3750/40) = 9.682 rad/s
fn = 9.682/(2π) = 1.541 Hz

Answer

fn = 1.541 Hz

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