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MCEN90014 · Materials Engineering

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Chapter 3 of 12 · MCEN90014

Mechanical Properties of Metals & Ceramics

Mechanical properties is the Week 2 core of MCEN90014 Materials Engineering at the University of Melbourne, where the tensile stress–strain curve becomes your toolkit for stiffness, strength, ductility and energy. It sits on the subject's Process→Structure→Property spine and feeds directly into fracture, fatigue and failure analysis later in the course. Master this chapter and the metals-and-ceramics half of the final exam becomes a matter of reading one diagram correctly.

In this chapter

What this chapter covers

  • 01Define engineering stress σ = F/A₀ and engineering strain ε = ΔL/L₀ with correct units
  • 02Use Hooke's law σ = Eε and read Young's modulus E as the slope of the elastic line
  • 03Apply Poisson's ratio ν = −ε_lateral/ε_axial to find lateral contraction
  • 04Convert between engineering and true stress–strain (σ_T = σ(1+ε), ε_T = ln(1+ε))
  • 05Quantify ductility with percent elongation (%EL) and reduction in area (%RA)
  • 06Compute resilience (σ_y²/2E) and toughness (area under the whole curve)
  • 07Relate hardness to tensile strength (Callister σ_TS ≈ 3.45×HB; Vickers HV = 1.854P/d²)
  • 08Read a fatigue S–N curve and use amplitude, mean stress and the endurance limit
  • 09Contrast ductile metals with brittle, flaw-sensitive ceramics
Worked example · free

Elastic loading of an aluminium rod

Q [6 marks]. A round aluminium rod of diameter d = 12 mm and gauge length L₀ = 200 mm carries an axial tensile force F = 8.0 kN. For this alloy E = 70 GPa, the yield strength σ_y = 240 MPa and Poisson's ratio ν = 0.33. Find the stress, the extension and the change in diameter, and justify that the rod stays elastic.
  • +1Original area: A₀ = (π/4)d² = (π/4)(0.012)² = 1.131×10⁻⁴ m².
  • +1Engineering stress: σ = F/A₀ = 8000 / 1.131×10⁻⁴ = 7.07×10⁷ Pa = 70.7 MPa.
  • +1Elastic check: σ = 70.7 MPa < σ_y = 240 MPa, so the rod is in the linear-elastic region and Hooke's law plus Poisson's ratio apply.
  • +1Axial strain and extension: ε = σ/E = 70.7×10⁶ / 70×10⁹ = 1.01×10⁻³; ΔL = εL₀ = 1.01×10⁻³ × 200 = 0.202 mm, so L_f = 200.20 mm.
  • +1Lateral strain: ε_lat = −νε = −0.33 × 1.01×10⁻³ = −3.34×10⁻⁴.
  • +1Change in diameter: Δd = ε_lat·d = −3.34×10⁻⁴ × 12 = −4.0×10⁻³ mm, so the diameter contracts to d_f = 11.996 mm.
σ ≈ 70.7 MPa, extension ΔL ≈ 0.202 mm (L_f = 200.20 mm), and the diameter contracts by ≈ 0.004 mm to 11.996 mm. Because the applied stress is well below yield, the deformation is fully elastic and recoverable.
Sia tip — Always compare σ with σ_y before using Hooke's law or Poisson's ratio — those relations only hold in the elastic region. Carry SI units through every line so a MPa/Pa or mm/m slip cannot creep in.
Glossary

Key terms

Engineering stress (σ)
Applied force divided by the ORIGINAL cross-sectional area, σ = F/A₀, in pascals (1 MPa = 10⁶ Pa = 1 N/mm²).
Young's modulus (E)
The slope of the linear-elastic part of the stress–strain curve, σ = Eε; a stiffness set by bonding, in GPa. It barely changes with heat treatment or cold work.
Poisson's ratio (ν)
The magnitude ratio of lateral to axial strain, ν = −ε_lateral/ε_axial; dimensionless, ≈ 0.33 for metals and ≈ 0.25 for ceramics.
True stress–strain
Stress and strain based on the instantaneous area: σ_T = σ(1+ε), ε_T = ln(1+ε), valid up to necking. True stress keeps rising even after the engineering curve turns down.
Ductility
How much plastic strain a material sustains before fracture, measured as percent elongation %EL = (L_f−L₀)/L₀×100 or percent reduction in area %RA. Ductile is usually %EL > ~5%.
Resilience
Elastic energy stored per unit volume; the modulus of resilience is U_R = σ_y²/(2E) in J/m³ — the area under the elastic part of the curve.
Toughness
Total energy absorbed per unit volume up to fracture, the area under the WHOLE stress–strain curve. It needs both strength and ductility, so a strong-but-brittle material can have low toughness.
Endurance limit (σ_e)
On an S–N fatigue curve, a stress amplitude below which a steel survives effectively indefinitely (a horizontal asymptote). Many aluminium alloys have no endurance limit.
FAQ

Mechanical Properties of Metals & Ceramics FAQ

What is the difference between engineering and true stress–strain?

Engineering values use the original area and length (σ = F/A₀, ε = ΔL/L₀) — what the machine reports. True values use the instantaneous, shrinking area: σ_T = σ(1+ε) and ε_T = ln(1+ε), valid up to necking. The engineering curve dips after the tensile-strength peak because the specimen necks (a geometry effect), while the true stress needed to keep deforming keeps rising to fracture.

Why are ceramics tested in bending rather than tension?

Ceramics are brittle and flaw-sensitive — their strength is set by the largest crack, and they are far weaker in tension than in compression. Gripping a ceramic in tension tends to fail it at the grips, and the results scatter widely. A three-point bend test is easier to run and, with a statistical treatment of the scatter, gives a usable flexural strength (covered in the statistical-analysis chapter).

Can AI help me with mechanical properties in MCEN90014?

Yes — Sia is an AI tutor that can explain the concepts step by step: it can walk you through reading a stress–strain curve, show why the elastic check comes before Hooke's law, or check that your units are consistent in a worked problem. It is a study aid for understanding the method, not a source of ready-made answers, and it will not sit an assessment or guarantee a grade. Always follow the University of Melbourne's academic-integrity and generative-AI rules for MCEN90014 and confirm what is permitted on Canvas.

Studying with AI? Sia — free AI mechanical engineering tutor works through MCEN90014 step by step.

Study strategy

Exam move

Anchor everything to one drawing: sketch the stress–strain curve and label the elastic slope (E), the yield point (σ_y), the tensile-strength peak (σ_TS) and fracture, then note that resilience is the elastic-area and toughness the whole-area under it. Because a formula sheet is provided in the final exam, spend your practice time on choosing the right relation and substituting cleanly with SI units, not on memorising equations — the marks reward the elastic-vs-plastic justification and correct units as much as the final number. Re-derive a few problems by hand (an elastic rod with Poisson contraction, a true-stress conversion, a fatigue amplitude/mean pair) until the sign and factor conventions are automatic, since a reversed sign or a swapped amplitude/mean is the most common lost mark. The final exam is 10 questions of 10 marks each (100 marks, all compulsory) worth 50% of the subject with an exam hurdle, so treat every question as equally weighted and confirm the exam duration on the timetable in Canvas.

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