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
d1​ = 160 mmd2​ = 315 mm1440 rpmT1​ = 600 NT2​ = 120 NP = ?

A belt runs on a 160 mm driving pulley at 1440 rpm. The tension is 600 N on the tight side and 120 N on the slack side. Find the power P transmitted, in kW.

d1 = 160 mmn1 = 1440 rpmT1 = 600 NT2 = 120 N
P = kW
2.Gears & gear trainsHard
d1​ = 160 mmd2​ = 450 mm720 rpmC = 500 mmθ = ?

An open belt connects a 160 mm pulley and a 450 mm pulley whose centres are 500 mm apart. Find the angle of wrap θ on the smaller pulley, in degrees.

d1 = 160 mmd2 = 450 mmC = 500 mm
θ = °
3.Torsion of shaftsMedium
T = 750 N·md = 25 mmL = 1 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 = 750 N·md = 25 mmL = 1 mG = 80 GPa
φ = °
4.Torsion of shaftsHard
d = 40 mmTB​ = 1000 N·mTC​ = 1500 N·mABC0.8 m2.5 m

A solid steel shaft of diameter 40 mm is fixed at A. A torque of 1000 N·m acts at B, 0.8 m from A, and a torque of 1500 N·m in the opposite direction acts at the free end C, a further 2.5 m along. Find the magnitude of the angle of twist φC of end C, in degrees.

d = 40 mmTB = 1000 N·mTC = 1500 N·mAB = 0.8 mBC = 2.5 mG = 80 GPa
φC = °
5.Mohr’s circle & stress transformationMedium
σx​ = 50σy​ = 30τxy​ = 30MPa

A point in a loaded part has σₓ = 50 MPa, σᵧ = 30 MPa and τₓᵧ = 30 MPa (tension positive). Find the maximum in-plane shear stress τmax.

σx = 50 MPaσy = 30 MPaτxy = 30 MPa
τmax = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 120σy​ = 80τxy​ = 60MPa

A point in a loaded part has σₓ = 120 MPa, σᵧ = 80 MPa and τₓᵧ = 60 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 40° counter-clockwise from the x-axis (positive in the same sense as τₓᵧ).

σx = 120 MPaσy = 80 MPaτxy = 60 MPaθ = 40°
τθ = MPa
7.Axial stress & strainMedium
150 kNØ20110 GPaØ100/50300 mmδ = ?

A steel rod (diameter 20 mm, E = 200 GPa) sits inside a tube made of bronze (outer diameter 100 mm, inner diameter 50 mm, E = 110 GPa). Both are 300 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/Ø50 mm, E = 110 GPaL = 300 mm
δ = mm
8.Axial stress & strainHard
P = ?Ø40110 GPaØ100/60400 mm

A steel rod (diameter 40 mm, E = 200 GPa, allowable stress 150 MPa) sits inside a tube made of bronze (outer diameter 100 mm, inner diameter 60 mm, E = 110 GPa, allowable stress 70 MPa). They are compressed together between rigid plates. Find the largest load Pmax.

rod: Ø40 mm, E = 200 GPa, σallow = 150 MPatube: Ø100/Ø60 mm, E = 110 GPa, σallow = 70 MPa
Pmax = kN
9.Column bucklingMedium
PL = 4 m30 × 100 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 = 4 mE = 70 GPa (aluminium)b × h = 30 × 100 mm
Pcr = kN
10.Column bucklingHard
PL = 5 md = 40 mmcross-section

A column of length L made of aluminium is fixed at the base and pinned at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 5 mE = 70 GPa (aluminium)d = 40 mm
σcr = MPa
11.Mechanical vibrationsMedium
k = 100 kN/mc = 5660 N·s/mm = 500 kg

A 500 kg mass is supported by a spring with a stiffness of 100 kN/m and a viscous damper with a damping coefficient of 5660 N·s/m. Find the damping ratio ζ.

m = 500 kgk = 100 kN/mc = 5660 N·s/m
ζ =
12.Mechanical vibrationsHard
k1​ = 30k2​ = 30k3​ = 50m = 100 kg

A 100 kg mass hangs from spring k₃ = 50 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 30 kN/m and k₂ = 30 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 = 100 kgk1 = 30 kN/mk2 = 30 kN/mk3 = 50 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: P = 5.791 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.

Belt speed

v = 12.06 m/s

Power

P = (600 − 120)·12.06 = 5791 W = 5.791 kW

Answer

P = 5.791 kW
2.Gears & gear trains

Answer: θ = 146.3 °

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(0.29) = 16.86°

Angle of wrap

θ = 180 − 2·16.86 = 146.3°

Answer

θ = 146.3°
3.Torsion of shafts

Answer: φ = 14.01 °

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·25⁴/32 = 38350 mm⁴

Angle of twist

φ = TL/(GJ) = 750·1000·1000/(80000·38350) = 0.2445 rad
φ = 0.2445·180/π = 14.01°

Answer

φ = 14.01°
4.Torsion of shafts

Answer: φC = 11.83 °

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 = 1500 N·m
TAB = TC − TB = 1500 − 1000 = 500 N·m

Twist of each segment

J = π·40⁴/32 = 251327 mm⁴
G = 80 GPa = 80000 MPa
φAB = 500000·800/(80000·251327) = 0.01989 rad
φBC = 1.5 × 10⁶·2500/(80000·251327) = 0.1865 rad

Twist of end C

φC = 0.01989 + 0.1865 = 0.2064 rad → |φC| = 11.83°

Answer

φC = 11.83°
5.Mohr’s circle & stress transformation

Answer: τmax = 31.62 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 = √(((50 − 30)/2)² + 30²) = 31.62 MPa

Answer

τmax = 31.62 MPa
6.Mohr’s circle & stress transformation

Answer: τθ = −9.277 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.

Transformation equation

τθ = −20·0.9848 + 60·0.1736 = −9.277 MPa

Answer

τθ = −9.277 MPa
7.Axial stress & strain

Answer: δ = 0.06331 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 − 50²)/4 = 5890 mm²

Combined axial stiffness

ΣEA = 200·10³·314.2 + 110·10³·5890 = 7.108 × 10⁸ N

Shortening

δ = 150000·300/7.108 × 10⁸ = 0.06331 mm

Answer

δ = 0.06331 mm
8.Axial stress & strain

Answer: Pmax = 511.8 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·40²/4 = 1257 mm²
At = π(100² − 60²)/4 = 5027 mm²

Combined axial stiffness

ΣEA = 200·10³·1257 + 110·10³·5027 = 8.042 × 10⁸ N

Governing strain

ε = min(0.00075, 0.0006364) = 0.0006364 (bronze)

Largest load

Pmax = 0.0006364·8.042 × 10⁸ = 511794 N = 511.8 kN

Answer

Pmax = 511.8 kN
9.Column buckling

Answer: Pcr = 9.715 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 = 100·30³/12 = 225000 mm⁴

Effective length

KL = 1·4000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·225000/4000² = 9715 N = 9.715 kN

Answer

Pcr = 9.715 kN
10.Column buckling

Answer: σcr = 5.64 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·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 0.7·5000 = 3500 mm
KL/r = 3500/10 = 350

Critical stress

σcr = π²E/(KL/r)² = π²·70000/350² = 5.64 MPa

Answer

σcr = 5.64 MPa
11.Mechanical vibrations

Answer: ζ = 0.4002

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·√(100000·500) = 14142 N·s/m

Damping ratio

ζ = c/cc = 5660/14142 = 0.4002

Answer

ζ = 0.4002

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

12.Mechanical vibrations

Answer: fn = 2.628 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 = 30 + 30 = 60 kN/m
keq = 60·50/(60 + 50) = 27.27 kN/m

Natural frequency

ωn = √(27273/100) = 16.51 rad/s
fn = 16.51/(2π) = 2.628 Hz

Answer

fn = 2.628 Hz

ExamProblems · examproblems.com/courses/machine-design