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​ = 12N2​ = 72

A 1.1 kW motor running at 1450 rpm drives a pinion with 12 teeth, which meshes with a gear with 72 teeth. The gear pair has an efficiency of 98%. Find the torque T1 on the motor shaft.

P = 1.1 kWn1 = 1450 rpmN1 = 12N2 = 72η = 98%
T1 = N·m
2.Gears & gear trainsHard
A = 25B = 30C = 36D = 50

A 7.5 kW motor at 2900 rpm drives gear A (25 teeth), which meshes with gear B (30 teeth). Gear C (36 teeth) on the same shaft as B drives gear D (50 teeth) on the output shaft. Each gear mesh has an efficiency of 98%. Find the output torque Tout.

P = 7.5 kWnin = 2900 rpmA = 25B = 30C = 36D = 50ηmesh = 98%
Tout = N·m
3.Torsion of shaftsMedium
d = ?T = 1000 N·mL = 1.5 m

A solid steel shaft 1.5 m long carries a torque of 1000 N·m. The angle of twist between its ends must not exceed 1°. Find the smallest diameter d that meets this limit.

T = 1000 N·mL = 1.5 mG = 80 GPaφallow = 1°
d = mm
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 5 kW at 1800 rpm without the shear stress exceeding 60 MPa. Find the smallest diameter d that works.

P = 5 kWN = 1800 rpmτallow = 60 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 50σy​ = 20τxy​ = −50MPa

A point in a loaded part has σₓ = 50 MPa, σᵧ = 20 MPa and τₓᵧ = −50 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = 50 MPaσy = 20 MPaτxy = −50 MPa
θp = °
6.Mohr’s circle & stress transformationHard
25°D = 500 mm, t = 5 mm, p = 1.5 MPap

A thin-walled cylindrical tank of inner diameter 500 mm and wall thickness 5 mm holds gas at a gauge pressure of 1.5 MPa. It is made from plate welded along a helical seam at 25° to the axis of the cylinder. Find the normal stress σn acting across the weld seam.

D = 500 mmt = 5 mmp = 1.5 MPaα = 25°
σn = MPa
7.Axial stress & strainMedium
Ø 16 mmBrass2 mP = 120 kN

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

P = 120 kNd = 16 mmL = 2 mE = 100 GPa
ε = µε
8.Axial stress & strainHard
Ø 40 mmSteel2 mØ 12 mmAluminium0.5 mP = 70 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 = 70 kNsegment 1: Ø40 mm, 2 m, steel (E = 200 GPa)segment 2: Ø12 mm, 0.5 m, aluminium (E = 70 GPa)
σmax = MPa
9.Column bucklingMedium
PL = 5 m40 × 100 mmcross-section

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

L = 5 mE = 200 GPa (steel)b × h = 40 × 100 mm
Pcr = kN
10.Column bucklingHard
P = 10 kNL = 6 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 10 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 10 kNn = 2.5L = 6 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
k = 25 kN/mζ = 0.5m = 8 kg

An 8 kg mass on a spring with a stiffness of 25 kN/m has a viscous damper giving a damping ratio of 0.5. Find the damped natural frequency fd of its free vibration in Hz.

m = 8 kgk = 25 kN/mζ = 0.5
fd = Hz
12.Mechanical vibrationsHard
k1​ = 25k2​ = 80m = 40 kg

A 40 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 25 kN/m and k₂ = 80 kN/m. The mass stays level. Find the equivalent stiffness keq of the spring system in kN/m.

m = 40 kgk1 = 25 kN/mk2 = 80 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: T1 = 7.244 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·1450/60 = 151.8 rad/s
T1 = P/ω₁ = 1100/151.8 = 7.244 N·m

Answer

T1 = 7.244 N·m
2.Gears & gear trains

Answer: Tout = 39.53 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.

Output speed

nout = 2900·(25/30)·(36/50) = 1740 rpm
ωout = 2π·1740/60 = 182.2 rad/s

Output power and torque

Pout = 7500·0.98² = 7203 W
Tout = Pout/ωout = 7203/182.2 = 39.53 N·m

Answer

Tout = 39.53 N·m
3.Torsion of shafts

Answer: d = 57.51 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.

Required polar moment

T = 1000 N·m = 1 × 10⁶ N·mm
L = 1.5 m = 1500 mm
G = 80 GPa = 80000 MPa
φ = 1·π/180 = 0.01745 rad
J = TL/(Gφ) = 1 × 10⁶·1500/(80000·0.01745) = 1.074 × 10⁶ mm⁴

Diameter

d = (32J/π)1/4 = 57.51 mm

Answer

d = 57.51 mm

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

4.Torsion of shafts

Answer: d = 13.11 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·1800/60 = 188.5 rad/s
T = P/ω = 5000/188.5 = 26.53 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·26526/(π·60)) = 13.11 mm

Answer

d = 13.11 mm

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

5.Mohr’s circle & stress transformation

Answer: θp = −36.65 °

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.

στxyCσ1​σ2​

Angle on the circle

Point x sits at an angle 2θp from the σ-axis on Mohr’s circle; the quadrant follows from the signs of σₓ − σᵧ and τₓᵧ.

2θp = atan2(2·−50, 50 − 20) = −73.3°

Angle on the element

θp = −36.65°

Answer

θp = −36.65°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: σn = 68.3 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 = 1.5·250/5 = 75 MPa
σa = pr/(2t) = 37.5 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 = 37.5·sin²25° + 75·cos²25° = 68.3 MPa

Answer

σn = 68.3 MPa
7.Axial stress & strain

Answer: ε = 5968 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·16²/4 = 201.1 mm²
σ = P/A = 120·1000/201.1 = 596.8 MPa

Strain (Hooke’s law)

E for brass = 100 GPa = 100000 MPa.

ε = σ/E = 596.8/100000 = 0.005968 = 5968 µε

Answer

ε = 5968 µε
8.Axial stress & strain

Answer: σmax = 618.9 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·40²/4 = 1257 mm², A2 = π·12²/4 = 113.1 mm²
σ1 = 55.7 MPa
σ2 = 618.9 MPa

Largest stress

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

σmax = 618.9 MPa

Answer

σmax = 618.9 MPa
9.Column buckling

Answer: Pcr = 168.4 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 = 100·40³/12 = 533333 mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·533333/2500² = 168441 N = 168.4 kN

Answer

Pcr = 168.4 kN
10.Column buckling

Answer: d = 55.21 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 = 2.5·10000 = 25000 N
KL = 1·6000 = 6000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·25000·6000²/(π³·200000))^(1/4) = 55.21 mm

Answer

d = 55.21 mm

Check: the slenderness KL/r is 434.7, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: fd = 7.705 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.

Undamped natural frequency

ωn = √(25000/8) = 55.9 rad/s
fn = 55.9/(2π) = 8.897 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 8.897·√(1 − 0.5²) = 7.705 Hz

Answer

fd = 7.705 Hz
12.Mechanical vibrations

Answer: keq = 105 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 side by side share the deflection and add their forces, so their stiffnesses simply add: k = k1 + k2.

keq = 25 + 80 = 105 kN/m

Answer

keq = 105 kN/m

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