FE Mechanics of Materials Practice Problems

Five original mechanics of materials problems in the style of the FE Mechanical exam, each with four answer choices and a full step-by-step solution: axial deformation, bending stress, principal stress, thermal stress and column buckling. Give yourself about 3 minutes per problem.

How to use these problems

Try each problem with a timer and your approved calculator before you open the solution. Keep units on every line; most wrong choices below come from a units slip or the wrong formula variant.

When you miss one, write down which formula you should have recognized, then find it in the FE Reference Handbook so you can find it faster next time.

Keep the mechanics of materials cheat sheet next to you while you study, then practise finding the same formulas in the FE Reference Handbook.

Practice problems

Problem 1: Elongation of a stepped rod

A steel rod has two segments: 0.80 m long with a 20 mm diameter, then 0.50 m long with a 12 mm diameter. It carries a 15 kN axial tension throughout. Take E = 200 GPa (typical for steel). What is the total elongation?

  1. 0.19 mm
  2. 0.33 mm
  3. 0.52 mm
  4. 0.62 mm
Show the solution to problem 1
  1. Areas of the two segments.A₁ = π(20)²/4 = 314.2 mm²; A₂ = π(12)²/4 = 113.1 mm²
  2. Elongation of each segment, δ = P·L/(A·E), with E = 200 000 N/mm².δ₁ = 15 000 × 800/(314.2 × 200 000) = 0.191 mm; δ₂ = 15 000 × 500/(113.1 × 200 000) = 0.332 mm
  3. Add them.δ = 0.191 + 0.332 = 0.52 mm

Answer: (C) 0.52 mm. Review: Stress and strain.

Problem 2: Bending stress in a timber beam

A simply supported beam spans 3.0 m and carries a uniform load of 5.0 kN/m (including its own weight). The cross-section is a solid rectangle 100 mm wide and 200 mm deep. What is the maximum bending stress?

  1. 8.4 MPa
  2. 2.1 MPa
  3. 16.9 MPa
  4. 33.8 MPa
Show the solution to problem 2
  1. Maximum moment at mid-span for a uniform load.M = w·L²/8 = 5.0 × 3.0²/8 = 5.625 kN·m
  2. Section modulus of the rectangle.S = b·h²/6 = 100 × 200²/6 = 666 700 mm³
  3. Flexure formula.σ = M/S = 5.625 × 10⁶ N·mm / 666 700 mm³ = 8.4 MPa

Answer: (A) 8.4 MPa. Review: Bending stress in beams.

Problem 3: Principal stress from plane stress

A point in a bracket has σ_x = 80 MPa, σ_y = −20 MPa and τ_xy = 30 MPa. What is the maximum principal stress σ₁?

  1. 80.0 MPa
  2. 58.3 MPa
  3. 110 MPa
  4. 88.3 MPa
Show the solution to problem 3
  1. Centre of Mohr’s circle.C = (80 + (−20))/2 = 30 MPa
  2. Radius.R = √[((80 − (−20))/2)² + 30²] = √(50² + 30²) = 58.3 MPa
  3. Maximum principal stress. Choice B is the radius, which is the maximum in-plane shear stress.σ₁ = C + R = 30 + 58.3 = 88.3 MPa

Answer: (D) 88.3 MPa. Review: Mohr’s circle.

Problem 4: Thermal stress in a restrained bar

An aluminum bar is fixed between two rigid walls with no gap and no initial stress. It is heated uniformly by 40 °C. Take E = 70 GPa and α = 23 × 10⁻⁶ /°C (typical for aluminum). What is the stress in the bar?

  1. 64.4 MPa tension
  2. 64.4 MPa compression
  3. 0; the bar is free to expand
  4. 0.92 MPa compression
Show the solution to problem 4
  1. The walls stop the bar from expanding, so the mechanical strain cancels the thermal strain.ε_thermal = α·ΔT = 23 × 10⁻⁶ × 40 = 920 × 10⁻⁶
  2. The stress needed to push the bar back to its original length.σ = E·α·ΔT = 70 000 MPa × 920 × 10⁻⁶ = 64.4 MPa
  3. The walls push on the bar, so the stress is compressive. The answer does not depend on the bar’s length or area.

Answer: (B) 64.4 MPa compression. Review: Thermal stress and expansion.

Problem 5: Buckling load of a pinned column

A solid round steel column, 30 mm in diameter and 1.5 m long, is pinned at both ends. Take E = 200 GPa (typical for steel). What is the Euler critical buckling load?

  1. 8.7 kN
  2. 34.9 kN
  3. 140 kN
  4. 69.8 kN
Show the solution to problem 5
  1. Moment of inertia of the round section.I = π·d⁴/64 = π × 30⁴/64 = 39 760 mm⁴
  2. Pinned at both ends, so the effective-length factor is K = 1.K·L = 1 500 mm
  3. Euler formula. Choice A uses K = 2 and choice C uses K = 0.5.P_cr = π²·E·I/(K·L)² = π² × 200 000 × 39 760 / 1 500² = 34 900 N
  4. Check that Euler applies: the stress at buckling is well below the yield strength of structural steel.σ_cr = 34 900/706.9 = 49 MPa

Answer: (B) 34.9 kN. Review: Column buckling.

Frequently asked questions

Are these real FE exam questions?

No. They are original problems written for this page, in the multiple-choice style of the exam. NCEES does not release its exam questions.

How many mechanics of materials questions are on the FE Mechanical exam?

The NCEES FE Mechanical specification lists 9–14 mechanics of materials questions out of 110.

Which formulas should I be fastest at finding?

Axial deformation, the flexure formula, torsion, Mohr’s circle and Euler buckling come up repeatedly. Know what each one looks like in the handbook.

See also

More FE exam resources

Sources

  1. Fundamentals of Engineering (FE) Mechanical CBT Exam Specifications (effective beginning with the July 2020 examinations), NCEES
  2. J. M. Gere, B. J. Goodno, Mechanics of Materials, Cengage
  3. R. C. Hibbeler, Mechanics of Materials, Pearson

Last updated

COPLAIN AI PLATFORM

Generate yours automatically from your existing docs

Heading into manufacturing? Coplain turns engineering procedures into clear, audit-ready work instructions and job aids for the shop floor.

Generate yours automatically with Coplain →