Machine Design: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

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​ = 72

A 3 kW motor running at 960 rpm drives a pinion with 20 teeth, which meshes with a gear with 72 teeth. Ignore losses. Find the output torque T2 on the gear shaft.

P = 3 kWn1 = 960 rpmN1 = 20N2 = 72η = 100%
T2 = N·m
2.Gears & gear trainsHard
Ns​ = 24nr​ = ?Np​ = 20carrier fixed

In a planetary gear set the sun gear has 24 teeth and each planet gear has 20 teeth. The planet carrier is held fixed and the sun is driven at 1800 rpm. Find the speed nr of the ring gear (magnitude).

Ns = 24Np = 20ns = 1800 rpm
nr = rpm
3.Torsion of shaftsMedium
T = 400 N·md = 40 mmL = 2 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 = 400 N·md = 40 mmL = 2 mG = 80 GPa
φ = °
4.Torsion of shaftsHard
do​ = ?75 kW, 1000 rpm

A hollow shaft must transmit 75 kW at 1000 rpm. Its inner diameter is to be 0.8 times its outer diameter, and the shear stress must not exceed 50 MPa. Find the smallest outer diameter do.

P = 75 kWN = 1000 rpmdi/do = 0.8τallow = 50 MPa
do = mm
5.Mohr’s circle & stress transformationMedium
σx​ = 120σy​ = −80τxy​ = −40MPa

A point in a loaded part has σₓ = 120 MPa, σᵧ = −80 MPa and τₓᵧ = −40 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = 120 MPaσy = −80 MPaτxy = −40 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
20°D = 1000 mm, t = 8 mm, p = 1.2 MPap

A thin-walled cylindrical tank of inner diameter 1000 mm and wall thickness 8 mm holds gas at a gauge pressure of 1.2 MPa. It is made from plate welded along a helical seam at 20° to the axis of the cylinder. Find the magnitude of the shear stress |τn| acting along the weld seam.

D = 1000 mmt = 8 mmp = 1.2 MPaα = 20°
|τn| = MPa
7.Axial stress & strainMedium
80 kNØ30100 GPaØ80/60500 mmδ = ?

A steel rod (diameter 30 mm, E = 200 GPa) sits inside a tube made of brass (outer diameter 80 mm, inner diameter 60 mm, E = 100 GPa). Both are 500 mm long and are compressed together between rigid plates by 80 kN. Find the shortening δ.

P = 80 kNrod: Ø30 mm, E = 200 GPatube: Ø80/Ø60 mm, E = 100 GPaL = 500 mm
δ = mm
8.Axial stress & strainHard
P = ?Ø20110 GPaØ120/70800 mm

A steel rod (diameter 20 mm, E = 200 GPa, allowable stress 160 MPa) sits inside a tube made of bronze (outer diameter 120 mm, inner diameter 70 mm, E = 110 GPa, allowable stress 70 MPa). They are compressed together between rigid plates. Find the largest load Pmax.

rod: Ø20 mm, E = 200 GPa, σallow = 160 MPatube: Ø120/Ø70 mm, E = 110 GPa, σallow = 70 MPa
Pmax = kN
9.Column bucklingMedium
PL = 2.5 m25 × 80 mmcross-section

A column of length L made of aluminium is fixed at both ends. Using Euler’s formula, find its critical buckling load Pcr.

L = 2.5 mE = 70 GPa (aluminium)b × h = 25 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 110 kNL = 2 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 110 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 110 kNn = 2.5L = 2 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
k = 15 kN/mζ = 0.7m = 25 kg

A 25 kg mass on a spring with a stiffness of 15 kN/m has a viscous damper giving a damping ratio of 0.7. Find the damped natural frequency fd of its free vibration in Hz.

m = 25 kgk = 15 kN/mζ = 0.7
fd = Hz
12.Mechanical vibrationsHard
k1​ = 80k2​ = 12m = 10 kg

A 10 kg mass hangs from two springs connected end to end (in series): the upper spring has k₁ = 80 kN/m and the lower one k₂ = 12 kN/m. Find the equivalent stiffness keq of the spring system in kN/m.

m = 10 kgk1 = 80 kN/mk2 = 12 kN/m
keq = kN/m

3Solutions

1.Gears & gear trains

Answer: T2 = 107.4 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 = 3000/100.5 = 29.84 N·m

Output torque

T2 = 29.84·72/20·1 = 107.4 N·m

Answer

T2 = 107.4 N·m
2.Gears & gear trains

Answer: nr = 675 rpm

Planetary gear sets: the speeds of sun, ring and carrier are linked by the Willis equation (ns − nc)/(nr − nc) = −Nr/Ns: seen from the carrier, the set is an ordinary train with the planets as idlers. Holding one member fixed turns the set into a single-ratio reducer.

Ring gear teeth

Nr = Ns + 2·Np = 24 + 2·20 = 64

Willis equation with the carrier fixed

With nc = 0 the sun drives the ring through the planets, which act as idlers.

nr = −ns·Ns/Nr = −1800·24/64 = −675 rpm
|nr| = 675 rpm

Answer

nr = 675 rpm

The ring turns opposite to the sun.

3.Torsion of shafts

Answer: φ = 2.28 °

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·40⁴/32 = 251327 mm⁴

Angle of twist

φ = TL/(GJ) = 400·1000·2000/(80000·251327) = 0.03979 rad
φ = 0.03979·180/π = 2.28°

Answer

φ = 2.28°
4.Torsion of shafts

Answer: do = 49.81 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·1000/60 = 104.7 rad/s
T = P/ω = 75000/104.7 = 716.2 N·m

Outer diameter from the allowable stress

T = 716.2 N·m = 716197 N·mm
1 − k⁴ = 1 − 0.8⁴ = 0.5904
do = ∛(16T/(π·τallow·(1 − k⁴))) = ∛(16·716197/(π·50·0.5904)) = 49.81 mm
di = 0.8·49.81 = 39.85 mm

Answer

do = 49.81 mm

A solid shaft would need d = 41.78 mm; the hollow one is a little larger but much lighter.

5.Mohr’s circle & stress transformation

Answer: τmax = 107.7 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 = √(((120 − −80)/2)² + −40²) = 107.7 MPa

Answer

τmax = 107.7 MPa
6.Mohr’s circle & stress transformation

Answer: |τn| = 12.05 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. Thin-walled cylinder: hoop stress σh = pr/t and axial stress σa = pr/(2t); these are the principal stresses in the wall.

Wall stresses

r = 1000/2 = 500 mm
σh = pr/t = 1.2·500/8 = 75 MPa
σa = pr/(2t) = 37.5 MPa

Transform to the seam

Take x along the axis (σa) and y around the hoop (σh). The seam’s normal makes 90° − α with the axis.

|τn| = (75 − 37.5)·sin 20°·cos 20° = 12.05 MPa

Answer

|τn| = 12.05 MPa
7.Axial stress & strain

Answer: δ = 0.1107 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·30²/4 = 706.9 mm²
At = π(80² − 60²)/4 = 2199 mm²

Combined axial stiffness

ΣEA = 200·10³·706.9 + 100·10³·2199 = 3.613 × 10⁸ N

Shortening

δ = 80000·500/3.613 × 10⁸ = 0.1107 mm

Answer

δ = 0.1107 mm
8.Axial stress & strain

Answer: Pmax = 562.3 kN

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(120² − 70²)/4 = 7461 mm²

Combined axial stiffness

ΣEA = 200·10³·314.2 + 110·10³·7461 = 8.836 × 10⁸ N

Governing strain

ε = min(0.0008, 0.0006364) = 0.0006364 (bronze)

Largest load

Pmax = 0.0006364·8.836 × 10⁸ = 562274 N = 562.3 kN

Answer

Pmax = 562.3 kN
9.Column buckling

Answer: Pcr = 46.06 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 = 80·25³/12 = 104167 mm⁴

Effective length

KL = 0.5·2500 = 1250 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·104167/1250² = 46058 N = 46.06 kN

Answer

Pcr = 46.06 kN
10.Column buckling

Answer: d = 41.04 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 = 2.5·110000 = 275000 N
KL = 0.5·2000 = 1000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·275000·1000²/(π³·200000))^(1/4) = 41.04 mm

Answer

d = 41.04 mm

Check: the slenderness KL/r is 97.45, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: fd = 2.784 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.

Undamped natural frequency

ωn = √(15000/25) = 24.49 rad/s
fn = 24.49/(2π) = 3.898 Hz

Damped natural frequency

fd = fn·√(1 − ζ²) = 3.898·√(1 − 0.7²) = 2.784 Hz

Answer

fd = 2.784 Hz
12.Mechanical vibrations

Answer: keq = 10.43 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 = 1/80 + 1/12 → keq = 80·12/(80 + 12) = 10.43 kN/m

Answer

keq = 10.43 kN/m

ExamProblems · examproblems.com/courses/machine-design