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​N2​ = ?

Two parallel shafts are 125 mm apart. They must be connected by a pair of spur gears with a module of 5 mm and a speed reduction of 1.5 : 1. How many teeth N2 must the gear have?

a = 125 mmm = 5 mmi = 1.5
N2 =
2.Gears & gear trainsHard
A = 18B = 25C = 16D = 36

In a compound gear train, gear A (18 teeth) on the input shaft turning at 2900 rpm drives gear B (25 teeth). Gear C (16 teeth) is fixed to the same shaft as B and drives gear D (36 teeth) on the output shaft. Find the output speed nout.

nin = 2900 rpmA = 18B = 25C = 16D = 36
nout = rpm
3.Torsion of shaftsMedium
do​ = 50, di​ = 30 mmT = 400 N·mL = 1 m

A hollow brass shaft (outer diameter 50 mm, inner diameter 30 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 = 50 mmdi = 30 mmL = 1 mG = 39 GPa
φ = °
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 10 kW at 3000 rpm without the shear stress exceeding 75 MPa. Find the smallest diameter d that works.

P = 10 kWN = 3000 rpmτallow = 75 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = −30σy​ = 40τxy​ = 60MPa

A point in a loaded part has σₓ = −30 MPa, σᵧ = 40 MPa and τₓᵧ = 60 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = −30 MPaσy = 40 MPaτxy = 60 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​τxy​surface of the shaft

A solid shaft of diameter 20 mm carries an axial compressive force of 100 kN together with a torque of 200 N·m. At the surface of the shaft, find the maximum in-plane shear stress τmax.

d = 20 mmF = −100 kNT = 200 N·m
τmax = MPa
7.Axial stress & strainMedium
Ø 10 mmSteel2.5 mP = 10 kN

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

P = 10 kNd = 10 mmL = 2.5 mE = 200 GPa
δ = mm
8.Axial stress & strainHard
Ø 35 mmCopper1.5 mØ 12 mmAluminium0.5 mP = 115 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 = 115 kNsegment 1: Ø35 mm, 1.5 m, copper (E = 117 GPa)segment 2: Ø12 mm, 0.5 m, aluminium (E = 70 GPa)
σmax = MPa
9.Column bucklingMedium
PL = 4 md = 50 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 = 4 mE = 200 GPa (steel)d = 50 mm
Pcr = kN
10.Column bucklingHard
PL = 1 md = 25 mmcross-section

A column of length L made of steel 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 mE = 200 GPa (steel)d = 25 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 1 kN/mc = 40 N·s/mm = 8 kg

An 8 kg mass is supported by a spring with a stiffness of 1 kN/m and a viscous damper with a damping coefficient of 40 N·s/m. Find the damping ratio ζ.

m = 8 kgk = 1 kN/mc = 40 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 20k2​ = 15m = 100 kg

A 100 kg mass hangs from two springs connected end to end (in series): the upper spring has k₁ = 20 kN/m and the lower one k₂ = 15 kN/m. Find the equivalent stiffness keq of the spring system in kN/m.

m = 100 kgk1 = 20 kN/mk2 = 15 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: N2 = 30

Gear geometry: the module m sets the tooth size. A gear with N teeth has a pitch diameter d = m·N, two meshing gears have the same module, and their centre distance is a = (d₁ + d₂)/2 = m·(N₁ + N₂)/2. The pitch-line speed is v = π·d·n/60, and the tangential tooth force follows from the torque: Ft = 2T/d.

Total number of teeth

N1 + N2 = 2a/m = 2·125/5 = 50

Split by the ratio

N1 = 50/(1 + 1.5) = 20
N2 = 1.5·20 = 30

Answer

N2 = 30
2.Gears & gear trains

Answer: nout = 928 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 = 2900·18/25 = 2088 rpm = nC

Second stage

nout = 2088·16/36 = 928 rpm

Answer

nout = 928 rpm

total ratio = 3.125 : 1

3.Torsion of shafts

Answer: φ = 1.1 °

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 − 30⁴)/32 = 534071 mm⁴

Angle of twist

T = 400 N·m = 400000 N·mm
L = 1 m = 1000 mm
G = 39 GPa = 39000 MPa
φ = TL/(GJ) = 400000·1000/(39000·534071) = 0.0192 rad
φ = 0.0192·180/π = 1.1°

Answer

φ = 1.1°
4.Torsion of shafts

Answer: d = 12.93 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·3000/60 = 314.2 rad/s
T = P/ω = 10000/314.2 = 31.83 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·31831/(π·75)) = 12.93 mm

Answer

d = 12.93 mm

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

5.Mohr’s circle & stress transformation

Answer: θp = 60.13 °

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(2·60, −30 − 40) = 120.3°

Angle on the element

θp = 60.13°

Answer

θp = 60.13°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: τmax = 203.8 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.

Stresses at the surface

σ = F/A = −100000/(π·20²/4) = −100000/314.2 = −318.3 MPa
τ = 16T/(πd³) = 16·200000/(π·20³) = 127.3 MPa
στxyCτmax​

Mohr’s circle

C = σ/2 = −159.2 MPa
R = √((−159.2)² + 127.3²) = 203.8 MPa

Answer

τmax = 203.8 MPa
7.Axial stress & strain

Answer: δ = 1.592 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·10²/4 = 78.54 mm²
σ = P/A = 10·1000/78.54 = 127.3 MPa

Strain (Hooke’s law)

E for steel = 200 GPa = 200000 MPa.

ε = σ/E = 127.3/200000 = 0.0006366 = 636.6 µε

Elongation

δ = ε·L = 0.0006366·2500 mm = 1.592 mm

Answer

δ = 1.592 mm
8.Axial stress & strain

Answer: σmax = 1017 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·12²/4 = 113.1 mm²
σ1 = 119.5 MPa
σ2 = 1017 MPa

Largest stress

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

σmax = 1017 MPa

Answer

σmax = 1017 MPa
9.Column buckling

Answer: Pcr = 77.24 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 = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·306796/2800² = 77244 N = 77.24 kN

Answer

Pcr = 77.24 kN
10.Column buckling

Answer: σcr = 19.28 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·25⁴/64 = 19175 mm⁴

Radius of gyration and slenderness

A = 490.9 mm²
r = √(I/A) = √(19175/490.9) = 6.25 mm
KL = 2·1000 = 2000 mm
KL/r = 2000/6.25 = 320

Critical stress

σcr = π²E/(KL/r)² = π²·200000/320² = 19.28 MPa

Answer

σcr = 19.28 MPa
11.Mechanical vibrations

Answer: ζ = 0.2236

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·√(1000·8) = 178.9 N·s/m

Damping ratio

ζ = c/cc = 40/178.9 = 0.2236

Answer

ζ = 0.2236

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

12.Mechanical vibrations

Answer: keq = 8.571 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 = 1/20 + 1/15 → keq = 20·15/(20 + 15) = 8.571 kN/m

Answer

keq = 8.571 kN/m

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