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
d1​ = 150 mmd2​ = 250 mm960 rpmn2​ = ?

A 150 mm pulley at 960 rpm drives a 250 mm pulley by a belt with 2.5 % slip. Find the speed n2 of the driven pulley.

n1 = 960 rpmd1 = 150 mmd2 = 250 mms = 2.5 %
n2 = rpm
2.Gears & gear trainsHard
d1​ = 100 mmd2​ = 500 mm2880 rpmC = 600 mmT1​ = 500 NT2​P = ?

An open belt connects a 100 mm driving pulley at 2880 rpm to a 500 mm pulley; the centres are 600 mm apart. The coefficient of friction is 0.3 and the tight-side tension may not exceed 500 N. Find the largest power P the belt can transmit without slipping, in kW (ignore centrifugal effects).

d1 = 100 mmn1 = 2880 rpmd2 = 500 mmC = 600 mmμ = 0.3T1 = 500 N
P = kW
3.Torsion of shaftsMedium
d = ?T = 2000 N·mL = 1.5 m

A solid steel shaft 1.5 m long carries a torque of 2000 N·m. The angle of twist between its ends must not exceed 3°. Find the smallest diameter d that meets this limit.

T = 2000 N·mL = 1.5 mG = 80 GPaφallow = 3°
d = mm
4.Torsion of shaftsHard
do​ = ?100 kW, 1450 rpm

A hollow shaft must transmit 100 kW at 1450 rpm. Its inner diameter is to be 0.75 times its outer diameter, and the shear stress must not exceed 75 MPa. Find the smallest outer diameter do.

P = 100 kWN = 1450 rpmdi/do = 0.75τallow = 75 MPa
do = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 0σy​ = 0τxy​ = −40MPa

A point in a loaded part has σₓ = 0 MPa, σᵧ = 0 MPa and τₓᵧ = −40 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = 0 MPaσy = 0 MPaτxy = −40 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σy​ = 60τxy​ = 30MPa

A point in a thin plate is in plane stress: σₓ = 0 MPa, σᵧ = 60 MPa and τₓᵧ = 30 MPa (σz = 0). The material has a yield strength of 275 MPa. Find the factor of safety n against yielding by the von Mises (distortion energy) criterion.

σx = 0 MPaσy = 60 MPaτxy = 30 MPaσY = 275 MPa
n =
7.Axial stress & strainMedium
150 kNØ20100 GPaØ100/70500 mmδ = ?

A steel rod (diameter 20 mm, E = 200 GPa) sits inside a tube made of brass (outer diameter 100 mm, inner diameter 70 mm, E = 100 GPa). Both are 500 mm long and are compressed together between rigid plates by 150 kN. Find the shortening δ.

P = 150 kNrod: Ø20 mm, E = 200 GPatube: Ø100/Ø70 mm, E = 100 GPaL = 500 mm
δ = mm
8.Axial stress & strainHard
Ø 25 mmAluminium1 mØ 16 mmSteel1.5 mP = 115 kN

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

P = 115 kNsegment 1: Ø25 mm, 1 m, aluminium (E = 70 GPa)segment 2: Ø16 mm, 1.5 m, steel (E = 200 GPa)
δ = mm
9.Column bucklingMedium
PL = 2 m50 × 80 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 = 2 mE = 70 GPa (aluminium)b × h = 50 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 20 kNL = 5 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 20 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 20 kNn = 2.5L = 5 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
k = 2 kN/mc = 80 N·s/mm = 20 kg

A 20 kg mass is supported by a spring with a stiffness of 2 kN/m and a viscous damper with a damping coefficient of 80 N·s/m. Find the damping ratio ζ.

m = 20 kgk = 2 kN/mc = 80 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 20k2​ = 5k3​ = 100m = 10 kg

A 10 kg mass hangs from spring k₃ = 100 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 20 kN/m and k₂ = 5 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 = 10 kgk1 = 20 kN/mk2 = 5 kN/mk3 = 100 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: n2 = 561.6 rpm

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.

Speed without slip

960·150/250 = 576 rpm

With slip

n2 = 576·0.975 = 561.6 rpm

Answer

n2 = 561.6 rpm
2.Gears & gear trains

Answer: P = 3.937 kW

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.

Angle of wrap

θ = 2.462 rad

Slack-side tension

eμθ = e0.7386 = 2.093, T₂ = 500/2.093 = 238.9 N

Power

P = (500 − 238.9)·15.08 = 3.937 kW

Answer

P = 3.937 kW
3.Torsion of shafts

Answer: d = 51.97 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 = 2000 N·m = 2 × 10⁶ N·mm
L = 1.5 m = 1500 mm
G = 80 GPa = 80000 MPa
φ = 3·π/180 = 0.05236 rad
J = TL/(Gφ) = 2 × 10⁶·1500/(80000·0.05236) = 716197 mm⁴

Diameter

d = (32J/π)1/4 = 51.97 mm

Answer

d = 51.97 mm

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

4.Torsion of shafts

Answer: do = 40.29 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·1450/60 = 151.8 rad/s
T = P/ω = 100000/151.8 = 658.6 N·m

Outer diameter from the allowable stress

T = 658.6 N·m = 658572 N·mm
1 − k⁴ = 1 − 0.75⁴ = 0.6836
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·658572/(π·75·0.6836)) = 40.29 mm
di = 0.75·40.29 = 30.22 mm

Answer

do = 40.29 mm

A solid shaft would need d = 35.5 mm; the hollow one is a little larger but much lighter.

5.Mohr’s circle & stress transformation

Answer: θp = −45 °

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·−40, 0 − 0) = −90°

Angle on the element

θp = −45°

Answer

θp = −45°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: n = 3.465

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 = 42.43 MPa
σ1 = 72.43 MPa, σ2 = −12.43 MPa, σ3 = 0

Von Mises

σvM = √(72.43² − 72.43·(−12.43) + (−12.43)²) = 79.37 MPa
n = 275/79.37 = 3.465

Answer

n = 3.465

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

7.Axial stress & strain

Answer: δ = 0.1619 mm

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.

Areas

Ar = π·20²/4 = 314.2 mm²
At = π(100² − 70²)/4 = 4006 mm²

Combined axial stiffness

ΣEA = 200·10³·314.2 + 100·10³·4006 = 4.634 × 10⁸ N

Shortening

δ = 150000·500/4.634 × 10⁸ = 0.1619 mm

Answer

δ = 0.1619 mm
8.Axial stress & strain

Answer: δ = 7.637 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 = 234.3 MPa
σ2 = 572 MPa

Add the segment elongations

δ1 = σ1L1/E1 = 234.3·1000/70000 = 3.347 mm
δ2 = σ2L2/E2 = 572·1500/200000 = 4.29 mm
δ = δ1 + δ2 = 7.637 mm

Answer

δ = 7.637 mm
9.Column buckling

Answer: Pcr = 143.9 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 = 80·50³/12 = 833333 mm⁴

Effective length

KL = 1·2000 = 2000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·833333/2000² = 143932 N = 143.9 kN

Answer

Pcr = 143.9 kN
10.Column buckling

Answer: d = 42.38 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 = 2.5·20000 = 50000 N
KL = 0.5·5000 = 2500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·50000·2500²/(π³·200000))^(1/4) = 42.38 mm

Answer

d = 42.38 mm

Check: the slenderness KL/r is 236, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.2

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·√(2000·20) = 400 N·s/m

Damping ratio

ζ = c/cc = 80/400 = 0.2

Answer

ζ = 0.2

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

12.Mechanical vibrations

Answer: fn = 7.118 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 = 20 + 5 = 25 kN/m
keq = 25·100/(25 + 100) = 20 kN/m

Natural frequency

ωn = √(20000/10) = 44.72 rad/s
fn = 44.72/(2π) = 7.118 Hz

Answer

fn = 7.118 Hz

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