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
Tw​ = ?z = 1, 960 rpm

A 1.1 kW motor at 960 rpm drives a worm with 1 start(s). The worm wheel has 45 teeth and the drive has an efficiency of 55%. Find the output torque Tw on the wheel shaft.

z = 1Nw = 45n = 960 rpmP = 1.1 kWη = 55%
Tw = N·m
2.Gears & gear trainsHard
A = 25B = 72C = 18D = ?

In a compound gear train, gear A (25 teeth) on the input shaft turns at 960 rpm and drives gear B (72 teeth). Gear C (18 teeth) is fixed to the same shaft as B and drives gear D on the output shaft. The output must turn at 120 rpm. How many teeth ND must gear D have?

nin = 960 rpmA = 25B = 72C = 18nout = 120 rpm
ND =
3.Torsion of shaftsMedium
T = 250 N·md = 20 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 = 250 N·md = 20 mmL = 0.5 mG = 39 GPa
φ = °
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 20 kW at 500 rpm without the shear stress exceeding 75 MPa. Find the smallest diameter d that works.

P = 20 kWN = 500 rpmτallow = 75 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 0σy​ = 110τxy​ = −10MPa

A point in a loaded part has σₓ = 0 MPa, σᵧ = 110 MPa and τₓᵧ = −10 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = 0 MPaσy = 110 MPaτxy = −10 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = −70σy​ = 10τxy​ = 20MPa

A point in a thin plate is in plane stress: σₓ = −70 MPa, σᵧ = 10 MPa and τₓᵧ = 20 MPa (σz = 0). The material has a yield strength of 355 MPa. Find the factor of safety n against yielding by the von Mises (distortion energy) criterion.

σx = −70 MPaσy = 10 MPaτxy = 20 MPaσY = 355 MPa
n =
7.Axial stress & strainMedium
Ø 16 mmAluminium3 mP = 75 kN

Find the elongation δ of the aluminium bar under the axial load.

P = 75 kNd = 16 mmL = 3 mE = 70 GPa
δ = mm
8.Axial stress & strainHard
Ø 40 mmSteel0.5 mØ 12 mmAluminium1 mP = 100 kN

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

P = 100 kNsegment 1: Ø40 mm, 0.5 m, steel (E = 200 GPa)segment 2: Ø12 mm, 1 m, aluminium (E = 70 GPa)
δ = mm
9.Column bucklingMedium
PL = 4 m25 × 40 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 = 25 × 40 mm
Pcr = kN
10.Column bucklingHard
PL = 5 md = 80 mmcross-section

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

L = 5 mE = 70 GPa (aluminium)d = 80 mm
σcr = MPa
11.Mechanical vibrationsMedium
tx15 mm1 cycle10.3 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 15 mm is followed one cycle later by a peak of 10.3 mm. Find the damping ratio ζ.

x0 = 15 mmx1 = 10.3 mmn = 1
ζ =
12.Mechanical vibrationsHard
k1​ = 50k2​ = 50k3​ = 20m = 100 kg

A 100 kg mass hangs from spring k₃ = 20 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 50 kN/m and k₂ = 50 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 = 100 kgk1 = 50 kN/mk2 = 50 kN/mk3 = 20 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: Tw = 270.8 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.

Wheel speed

nw = n·z/Nw = 960·1/45 = 21.33 rpm

Output torque

ωw = 2π·21.33/60 = 2.234 rad/s
Tw = η·P/ωw = 0.55·1100/2.234 = 270.8 N·m

Answer

Tw = 270.8 N·m
2.Gears & gear trains

Answer: ND = 50

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.

Intermediate shaft speed

nB = nC = 960·25/72 = 333.3 rpm

Teeth on gear D

ND = C·nC/nout = 18·333.3/120 = 50

Answer

ND = 50
3.Torsion of shafts

Answer: φ = 11.69 °

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·20⁴/32 = 15708 mm⁴

Angle of twist

φ = TL/(GJ) = 250·1000·500/(39000·15708) = 0.204 rad
φ = 0.204·180/π = 11.69°

Answer

φ = 11.69°
4.Torsion of shafts

Answer: d = 29.6 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 = 20000/52.36 = 382 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·381972/(π·75)) = 29.6 mm

Answer

d = 29.6 mm

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

5.Mohr’s circle & stress transformation

Answer: τmax = 55.9 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 = √(((0 − 110)/2)² + −10²) = 55.9 MPa

Answer

τmax = 55.9 MPa
6.Mohr’s circle & stress transformation

Answer: n = 4.274

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 = −30 MPa, R = 44.72 MPa
σ1 = 14.72 MPa, σ2 = −74.72 MPa, σ3 = 0

Von Mises

σvM = √(14.72² − 14.72·(−74.72) + (−74.72)²) = 83.07 MPa
n = 355/83.07 = 4.274

Answer

n = 4.274

n > 1 means the point does not yield; Tresca is slightly more conservative than von Mises.

7.Axial stress & strain

Answer: δ = 15.99 mm

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 = 75·1000/201.1 = 373 MPa

Strain (Hooke’s law)

E for aluminium = 70 GPa = 70000 MPa.

ε = σ/E = 373/70000 = 0.005329 = 5329 µε

Elongation

δ = ε·L = 0.005329·3000 mm = 15.99 mm

Answer

δ = 15.99 mm
8.Axial stress & strain

Answer: δ = 12.83 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·40²/4 = 1257 mm², A2 = π·12²/4 = 113.1 mm²
σ1 = 79.58 MPa
σ2 = 884.2 MPa

Add the segment elongations

δ1 = σ1L1/E1 = 79.58·500/200000 = 0.1989 mm
δ2 = σ2L2/E2 = 884.2·1000/70000 = 12.63 mm
δ = δ1 + δ2 = 12.83 mm

Answer

δ = 12.83 mm
9.Column buckling

Answer: Pcr = 2.249 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 = 40·25³/12 = 52083 mm⁴

Effective length

KL = 1·4000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·52083/4000² = 2249 N = 2.249 kN

Answer

Pcr = 2.249 kN
10.Column buckling

Answer: σcr = 22.56 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·80⁴/64 = 2.011 × 10⁶ mm⁴

Radius of gyration and slenderness

A = 5027 mm²
r = √(I/A) = √(2.011 × 10⁶/5027) = 20 mm
KL = 0.7·5000 = 3500 mm
KL/r = 3500/20 = 175

Critical stress

σcr = π²E/(KL/r)² = π²·70000/175² = 22.56 MPa

Answer

σcr = 22.56 MPa
11.Mechanical vibrations

Answer: ζ = 0.05972

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 = (1/1)·ln(15/10.3) = 0.3759

Damping ratio

ζ = δ/√(4π² + δ²) = 0.3759/√(39.48 + 0.1413) = 0.05972

Answer

ζ = 0.05972
12.Mechanical vibrations

Answer: fn = 2.055 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 = 50 + 50 = 100 kN/m
keq = 100·20/(100 + 20) = 16.67 kN/m

Natural frequency

ωn = √(16667/100) = 12.91 rad/s
fn = 12.91/(2π) = 2.055 Hz

Answer

fn = 2.055 Hz

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