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 80 mm apart. They must be connected by a pair of spur gears with a module of 2 mm and a speed reduction of 4 : 1. How many teeth N2 must the gear have?

a = 80 mmm = 2 mmi = 4
N2 =
2.Gears & gear trainsHard
d1​ = 100 mmd2​ = 250 mm960 rpmC = 500 mmθ = ?

An open belt connects a 100 mm pulley and a 250 mm pulley whose centres are 500 mm apart. Find the angle of wrap θ on the smaller pulley, in degrees.

d1 = 100 mmd2 = 250 mmC = 500 mm
θ = °
3.Torsion of shaftsMedium
T = 500 N·md = 30 mmL = 1.5 mφ = ?

A solid steel 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 = 500 N·md = 30 mmL = 1.5 mG = 80 GPa
φ = °
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 100 kW at 500 rpm without the shear stress exceeding 50 MPa. Find the smallest diameter d that works.

P = 100 kWN = 500 rpmτallow = 50 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = −20σy​ = 60τxy​ = −10MPa

A point in a loaded part has σₓ = −20 MPa, σᵧ = 60 MPa and τₓᵧ = −10 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = −20 MPaσy = 60 MPaτxy = −10 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​ = −70σy​ = −80τxy​ = 10MPa

A point in a thin plate is in plane stress: σₓ = −70 MPa, σᵧ = −80 MPa and τₓᵧ = 10 MPa (σz = 0). The material has a yield strength of 460 MPa. Find the factor of safety n against yielding by the von Mises (distortion energy) criterion.

σx = −70 MPaσy = −80 MPaτxy = 10 MPaσY = 460 MPa
n =
7.Axial stress & strainMedium
Ø 10 mmBrass3 mP = 85 kN

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

P = 85 kNd = 10 mmL = 3 mE = 100 GPa
ε = µε
8.Axial stress & strainHard
80 kN12400 mm400 mmØ30Ø50σ2​ = ?

A steel segment (diameter 30 mm, length 400 mm, E = 200 GPa) and a segment made of brass (diameter 50 mm, length 400 mm, E = 100 GPa) are joined end to end and fixed between two rigid walls. An axial load of 80 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø30 mm, 400 mm, E = 200 GPasegment 2: brass, Ø50 mm, 400 mm, E = 100 GPaP = 80 kN
σ2 = MPa
9.Column bucklingMedium
PL = 1.5 md = 60 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 = 1.5 mE = 70 GPa (aluminium)d = 60 mm
Pcr = kN
10.Column bucklingHard
P = 140 kNL = 1.5 md = ?cross-section

A solid round column of length L made of aluminium is pinned at both ends. It must carry 140 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 140 kNn = 2L = 1.5 mE = 70 GPa (aluminium)
d = mm
11.Mechanical vibrationsMedium
tx30 mm1 cycle23.3 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 30 mm is followed one cycle later by a peak of 23.3 mm. Find the damping ratio ζ.

x0 = 30 mmx1 = 23.3 mmn = 1
ζ =
12.Mechanical vibrationsHard
k1​ = 30k2​ = 5m = 100 kg

A 100 kg mass hangs from two springs side by side (in parallel), with stiffnesses k₁ = 30 kN/m and k₂ = 5 kN/m. The mass stays level. Ignore damping and the masses of the springs. Find the natural frequency fn of vertical vibration in Hz.

m = 100 kgk1 = 30 kN/mk2 = 5 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: N2 = 64

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 = 2·80/2 = 80

Split by the ratio

N1 = 80/(1 + 4) = 16
N2 = 4·16 = 64

Answer

N2 = 64
2.Gears & gear trains

Answer: θ = 162.7 °

Belt drives: without slip, both pulleys have the same rim speed v = π·d·n/60, so n₁·d₁ = n₂·d₂ and the speed ratio is d₂/d₁. Slip s makes the driven pulley a little slower: n₂ = n₁·(d₁/d₂)·(1 − s). The power transmitted is P = (T₁ − T₂)·v, with T₁ the tension on the tight side and T₂ on the slack side. Friction limits the ratio of the tensions: T₁/T₂ = eμθ, where θ is the angle of wrap in radians on the smaller pulley; for an open belt θ = π − 2·asin((d₂ − d₁)/(2C)) with centre distance C.

Belt angle

asin(0.15) = 8.627°

Angle of wrap

θ = 180 − 2·8.627 = 162.7°

Answer

θ = 162.7°
3.Torsion of shafts

Answer: φ = 6.755 °

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·30⁴/32 = 79522 mm⁴

Angle of twist

φ = TL/(GJ) = 500·1000·1500/(80000·79522) = 0.1179 rad
φ = 0.1179·180/π = 6.755°

Answer

φ = 6.755°
4.Torsion of shafts

Answer: d = 57.94 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 = 100000/52.36 = 1910 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·1.91 × 10⁶/(π·50)) = 57.94 mm

Answer

d = 57.94 mm

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

5.Mohr’s circle & stress transformation

Answer: θp = −82.98 °

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·−10, −20 − 60) = −166°

Angle on the element

θp = −82.98°

Answer

θp = −82.98°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: n = 5.939

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.

σxyCσ1​σ2​

Principal stresses

C = −75 MPa, R = 11.18 MPa
σ1 = −63.82 MPa, σ2 = −86.18 MPa, σ3 = 0

Von Mises

σvM = √((−63.82)² − (−63.82)·(−86.18) + (−86.18)²) = 77.46 MPa
n = 460/77.46 = 5.939

Answer

n = 5.939

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

7.Axial stress & strain

Answer: ε = 10823 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·10²/4 = 78.54 mm²
σ = P/A = 85·1000/78.54 = 1082 MPa

Strain (Hooke’s law)

E for brass = 100 GPa = 100000 MPa.

ε = σ/E = 1082/100000 = 0.01082 = 10823 µε

Answer

ε = 10823 µε
8.Axial stress & strain

Answer: σ2 = 23.69 MPa

Two materials: in series (one after the other) every segment carries the same force and the elongations add: δ = P·Σ L/(E·A). In parallel (side by side between rigid plates) both parts shorten by the same amount, so their strains are equal: the stiffer part takes the larger share, Pi = P·EiAi/ΣEA, and σi = Ei·ε. A bar held between two rigid walls with a load at the junction is statically indeterminate: the two segments share the load in proportion to their stiffness k = EA/L.

Stiffnesses

k₁ = 200000·706.9/400 = 353429 N/mm
k₂ = 100000·1963/400 = 490874 N/mm

Share of segment 2

F2 = 80000·490874/844303 = 46512 N

Stress

σ2 = 46512/1963 = 23.69 MPa (compression)

Answer

σ2 = 23.69 MPa
9.Column buckling

Answer: Pcr = 48.83 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·60⁴/64 = 636173 mm⁴

Effective length

KL = 2·1500 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·636173/3000² = 48835 N = 48.83 kN

Answer

Pcr = 48.83 kN
10.Column buckling

Answer: d = 65.65 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 = 2·140000 = 280000 N
KL = 1·1500 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·280000·1500²/(π³·70000))^(1/4) = 65.65 mm

Answer

d = 65.65 mm

Check: the slenderness KL/r is 91.39, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.04019

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(30/23.3) = 0.2527

Damping ratio

ζ = δ/√(4π² + δ²) = 0.2527/√(39.48 + 0.06388) = 0.04019

Answer

ζ = 0.04019
12.Mechanical vibrations

Answer: fn = 2.978 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 side by side share the deflection and add their forces, so their stiffnesses simply add: k = k1 + k2.

keq = 30 + 5 = 35 kN/m

Natural frequency

ωn = √(35000/100) = 18.71 rad/s
fn = 18.71/(2π) = 2.978 Hz

Answer

fn = 2.978 Hz

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