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​ = 20N2​ = 32

A 0.75 kW motor running at 960 rpm drives a pinion with 20 teeth, which meshes with a gear with 32 teeth. The gear pair has an efficiency of 95%. Find the torque T1 on the motor shaft.

P = 0.75 kWn1 = 960 rpmN1 = 20N2 = 32η = 95%
T1 = N·m
2.Gears & gear trainsHard
A = 15B = 36C = 20D = 30

In a compound gear train, gear A (15 teeth) on the input shaft turning at 960 rpm drives gear B (36 teeth). Gear C (20 teeth) is fixed to the same shaft as B and drives gear D (30 teeth) on the output shaft. Find the output speed nout.

nin = 960 rpmA = 15B = 36C = 20D = 30
nout = rpm
3.Torsion of shaftsMedium
do​ = ?T = 500 N·m

A hollow shaft must carry a torque of 500 N·m. Its inner diameter is to be 0.7 times its outer diameter, and the shear stress must not exceed 40 MPa. Find the smallest outer diameter do.

T = 500 N·mdi/do = 0.7τallow = 40 MPa
do = mm
4.Torsion of shaftsHard
d = 50 mmTB​ = 250 N·mTC​ = 250 N·mABC0.8 m0.8 m

A solid brass shaft of diameter 50 mm is fixed at A. A torque of 250 N·m acts at B, 0.8 m from A, and a torque of 250 N·m in the same direction acts at the free end C, a further 0.8 m along. Find the maximum shear stress τmax in the shaft.

d = 50 mmTB = 250 N·mTC = 250 N·mAB = 0.8 mBC = 0.8 m
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = 160σy​ = −10τxy​ = 30MPa

A point in a loaded part has σₓ = 160 MPa, σᵧ = −10 MPa and τₓᵧ = 30 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = 160 MPaσy = −10 MPaτxy = 30 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​ = −30σy​ = 40τxy​ = −30MPa

A point in a thin plate is in plane stress: σₓ = −30 MPa, σᵧ = 40 MPa and τₓᵧ = −30 MPa (σz = 0). The material has a yield strength of 350 MPa. Find the factor of safety n against yielding by the Tresca (maximum shear stress) criterion.

σx = −30 MPaσy = 40 MPaτxy = −30 MPaσY = 350 MPa
n =
7.Axial stress & strainMedium
Ø 30 mmAluminium3 mP = 70 kN

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

P = 70 kNd = 30 mmL = 3 mE = 70 GPa
δ = mm
8.Axial stress & strainHard
Ø 25 mmSteel1 mØ 16 mmBrass1.5 mP = 30 kN

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

P = 30 kNsegment 1: Ø25 mm, 1 m, steel (E = 200 GPa)segment 2: Ø16 mm, 1.5 m, brass (E = 100 GPa)
δ = mm
9.Column bucklingMedium
PL = 2.5 md = 50 mmcross-section

A column of length L made of aluminium is fixed at the base and free at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 2.5 mE = 70 GPa (aluminium)d = 50 mm
Pcr = kN
10.Column bucklingHard
P = 145 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 145 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 145 kNn = 3L = 4 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
tx50 mm5 cycles26.7 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 50 mm is followed 5 cycles later by a peak of 26.7 mm. Find the damping ratio ζ.

x0 = 50 mmx5 = 26.7 mmn = 5
ζ =
12.Mechanical vibrationsHard
k1​ = 15k2​ = 12m = 50 kg

A 50 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 15 kN/m and k₂ = 12 kN/m. The mass stays level. Find the equivalent stiffness keq of the spring system in kN/m.

m = 50 kgk1 = 15 kN/mk2 = 12 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: T1 = 7.46 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·960/60 = 100.5 rad/s
T1 = P/ω₁ = 750/100.5 = 7.46 N·m

Answer

T1 = 7.46 N·m
2.Gears & gear trains

Answer: nout = 266.7 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 = 960·15/36 = 400 rpm = nC

Second stage

nout = 400·20/30 = 266.7 rpm

Answer

nout = 266.7 rpm

total ratio = 3.6 : 1

3.Torsion of shafts

Answer: do = 43.76 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.

Outer diameter from the allowable stress

T = 500 N·m = 500000 N·mm
1 − k⁴ = 1 − 0.7⁴ = 0.7599
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·500000/(π·40·0.7599)) = 43.76 mm
di = 0.7·43.76 = 30.63 mm

Answer

do = 43.76 mm

A solid shaft would need d = 39.93 mm; the hollow one is a little larger but much lighter.

4.Torsion of shafts

Answer: τmax = 20.37 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 + 250 = 500 N·m

Maximum shear stress

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

|T|max = 500 N·m
τmax = 16·500000/(π·50³) = 20.37 MPa

Answer

τmax = 20.37 MPa
5.Mohr’s circle & stress transformation

Answer: θp = 9.72 °

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(2·30, 160 − −10) = 19.44°

Angle on the element

θp = 9.72°

Answer

θp = 9.72°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: n = 3.796

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 = 5 MPa, R = 46.1 MPa
σ1 = 51.1 MPa, σ2 = −41.1 MPa, σ3 = 0

Tresca

σmax − σmin = 92.2 MPa
n = 350/92.2 = 3.796

Answer

n = 3.796

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

7.Axial stress & strain

Answer: δ = 4.244 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·30²/4 = 706.9 mm²
σ = P/A = 70·1000/706.9 = 99.03 MPa

Strain (Hooke’s law)

E for aluminium = 70 GPa = 70000 MPa.

ε = σ/E = 99.03/70000 = 0.001415 = 1415 µε

Elongation

δ = ε·L = 0.001415·3000 mm = 4.244 mm

Answer

δ = 4.244 mm
8.Axial stress & strain

Answer: δ = 2.544 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·25²/4 = 490.9 mm², A2 = π·16²/4 = 201.1 mm²
σ1 = 61.12 MPa
σ2 = 149.2 MPa

Add the segment elongations

δ1 = σ1L1/E1 = 61.12·1000/200000 = 0.3056 mm
δ2 = σ2L2/E2 = 149.2·1500/100000 = 2.238 mm
δ = δ1 + δ2 = 2.544 mm

Answer

δ = 2.544 mm
9.Column buckling

Answer: Pcr = 8.478 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·50⁴/64 = 306796 mm⁴

Effective length

KL = 2·2500 = 5000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·306796/5000² = 8478 N = 8.478 kN

Answer

Pcr = 8.478 kN
10.Column buckling

Answer: d = 92.06 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 = 3·145000 = 435000 N
KL = 1·4000 = 4000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·435000·4000²/(π³·200000))^(1/4) = 92.06 mm

Answer

d = 92.06 mm

Check: the slenderness KL/r is 173.8, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.01997

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 = (1/5)·ln(50/26.7) = 0.1255

Damping ratio

ζ = δ/√(4π² + δ²) = 0.1255/√(39.48 + 0.01574) = 0.01997

Answer

ζ = 0.01997
12.Mechanical vibrations

Answer: keq = 27 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 = 15 + 12 = 27 kN/m

Answer

keq = 27 kN/m

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