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Properties of Materials

Properties of Materials

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Board Coverage AQA Paper 1 | Edexcel CP1 | OCR (A) Paper 1 | CIE P1

The mechanical properties of materials — how they deform, stretch, compress, and break — are central to engineering and physics. This topic sits within the "Mechanics & Materials" strand on every A Level board.

1. Hooke's Law

When an elastic object such as a spring or wire is stretched, the extension is (up to a limit) proportional to the applied force.

F=kΔx\boxed{F = k\,\Delta x}

where FF is the applied force, kk is the spring constant (N m1^{-1}), and Δx\Delta x is the extension from the natural length.

Definition. The spring constant kk is the force per unit extension required to stretch an elastic object. A stiff spring has a large kk; a soft spring has a small kk.

Definition. The limit of proportionality is the point beyond which force is no longer proportional to extension — the straight-line region of the force-extension graph ends.

Definition. The elastic limit is the maximum force that can be applied such that the material returns to its original length when the force is removed. Beyond this point, the material undergoes permanent (plastic) deformation.

warning

warning For many materials (especially metals), the elastic limit lies slightly beyond the limit of proportionality. Between these two points the material still returns to its original shape, but FF and Δx\Delta x are no longer linearly related.

Springs in Series and Parallel

For two springs with spring constants k1k_1 and k2k_2:

Series (force is the same through both, extensions add):

LB1RB◆◆LBkseriesRB=1k1+1k2\frac◆LB◆1◆RB◆◆LB◆k_{\mathrm{series}}◆RB◆ = \frac{1}{k_1} + \frac{1}{k_2}

Parallel (extension is the same for both, forces add):

kparallel=k1+k2k_{\mathrm{parallel}} = k_1 + k_2

Details

Example A spring of constant 200200 N m1^{-1} is joined in series with a spring of constant 300300 N m1^{-1}. A 1010 N weight is hung from the combination. Find the total extension.

Answer. 1k=1200+1300=5600=1120\frac{1}{k} = \frac{1}{200} + \frac{1}{300} = \frac{5}{600} = \frac{1}{120}. So k=120k = 120 N m1^{-1}.

Extension: Δx=F/k=10/120=0.0833\Delta x = F/k = 10/120 = 0.0833 m =8.3= 8.3 cm.

2. Stress and Strain

Force and extension depend on the size of the sample. To compare materials independently of sample geometry, we use stress and strain.

Definition. Stress σ\sigma is the force per unit cross-sectional area:

σ=FA\boxed{\sigma = \frac{F}{A}}

Units: pascals (Pa), where 1  Pa=1  Nm21\;\mathrm{Pa} = 1\;\mathrm{N m}^{-2}. Typical values range from 106\sim 10^6 Pa for soft metals to 109\sim 10^9 Pa for steel.

Definition. Strain ε\varepsilon is the extension per unit original length:

ε=LBΔLRB◆◆LBLRB\boxed{\varepsilon = \frac◆LB◆\Delta L◆RB◆◆LB◆L◆RB◆}

Strain is dimensionless (a ratio). It is often expressed as a percentage.

Definition. Breaking stress is the stress at which a material fractures.

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info (stretching) and compressive stress (squashing). AQA and Edexcel typically focus on tensile loading. OCR (A) may ask about compressive stress-strain behaviour of brittle materials like concrete.

3. Young's Modulus

Definition. The Young's modulus EE of a material is the ratio of tensile stress to tensile strain, within the limit of proportionality:

E=LBσRB◆◆LBεRB=LBF/ARB◆◆LBΔL/LRB=LBFLRB◆◆LBAΔLRB\boxed{E = \frac◆LB◆\sigma◆RB◆◆LB◆\varepsilon◆RB◆ = \frac◆LB◆F/A◆RB◆◆LB◆\Delta L/L◆RB◆ = \frac◆LB◆FL◆RB◆◆LB◆A\,\Delta L◆RB◆}

Young's modulus is a measure of stiffness — the resistance of a material to elastic deformation under tensile loading. It has units of Pa (same as stress, since strain is dimensionless).

Typical Values

MaterialYoung's Modulus (GPa)Type
Rubber0.01–0.1Polymer
Polyethylene0.2–1.0Polymer
Concrete30Ceramic
Glass70Ceramic
Aluminium70Metal
Copper130Metal
Steel200Metal
Diamond1200Ceramic/Crystal
warning

Common Pitfall A high Young's modulus means the material is stiff, not necessarily strong. Glass is stiffer than rubber (E70E \approx 70 GPa vs 0.010.01 GPa) but rubber is tougher (absorbs more energy before breaking) because it can undergo much larger strains. Stiffness and strength are different properties.

Measuring Young's Modulus

A standard experiment uses a wire clamped at one end with masses hung from the other:

  1. Measure the wire's diameter with a micrometer (at several points, take an average) to find A=πd2/4A = \pi d^2/4.
  2. Measure the original length LL with a metre rule.
  3. Add known masses mm and record the extension ΔL\Delta L with a vernier scale or Searle's apparatus.
  4. Plot a graph of force F=mgF = mg against extension ΔL\Delta L.
  5. The gradient is k=F/ΔLk = F/\Delta L. Then E=kL/A=LBFLRB◆◆LBAΔLRBE = kL/A = \frac◆LB◆FL◆RB◆◆LB◆A\,\Delta L◆RB◆.

Alternatively, plot stress against strain — the gradient is EE directly.

Details

Worked Example A steel wire of diameter 0.500.50 mm and length 2.02.0 m extends by 1.21.2 mm when a 5050 N force is applied. Calculate Young's modulus.

Answer. A=π(0.50×103/2)2=1.96×107A = \pi(0.50 \times 10^{-3}/2)^2 = 1.96 \times 10^{-7} m2^2.

σ=F/A=50/1.96×107=2.55×108\sigma = F/A = 50 / 1.96 \times 10^{-7} = 2.55 \times 10^8 Pa.

ε=ΔL/L=1.2×103/2.0=6.0×104\varepsilon = \Delta L/L = 1.2 \times 10^{-3} / 2.0 = 6.0 \times 10^{-4}.

E=σ/ε=2.55×108/6.0×104=4.25×1011E = \sigma/\varepsilon = 2.55 \times 10^8 / 6.0 \times 10^{-4} = 4.25 \times 10^{11} Pa =425= 425 GPa.

(This is somewhat high for steel; typical values are 180–210 GPa — the discrepancy may indicate the wire has exceeded its limit of proportionality.)

Proof of Young's Modulus from Hooke's Law

Starting from Hooke's law in its force-extension form:

F=kΔxF = k\,\Delta x

Multiply both sides by L/(AΔx)L/(A\,\Delta x):

LBFLRB◆◆LBAΔxRB=kLA\frac◆LB◆FL◆RB◆◆LB◆A\,\Delta x◆RB◆ = \frac{kL}{A}

Define σ=F/A\sigma = F/A, ε=Δx/L\varepsilon = \Delta x/L:

LBσRB◆◆LBεRB=kLA=E\frac◆LB◆\sigma◆RB◆◆LB◆\varepsilon◆RB◆ = \frac{kL}{A} = E

Since kk, LL, and AA are all constants for a given sample (within the proportional limit), EE is a constant of the material — it does not depend on the dimensions of the sample. \square

4. Stress-Strain Graphs

The stress-strain graph is the most important tool for characterising the mechanical behaviour of a material.

Regions of the Graph

  1. Linear (elastic) region — from origin to limit of proportionality. Stress is proportional to strain; gradient =E= E.
  2. Elastic region (non-linear) — between limit of proportionality and elastic limit. The material still returns to its original shape, but stress and strain are no longer proportional.
  3. Plastic region — beyond the elastic limit. Permanent deformation occurs. The material does not fully recover on unloading.
  4. Yield point — the stress at which plastic deformation begins (well-defined in mild steel; gradual in copper).
  5. Ultimate tensile strength (UTS) — the maximum stress the material can withstand.
  6. Breaking point (fracture) — the stress at which the material breaks.

Ductile Materials (e.g., Steel, Copper)

A ductile material undergoes significant plastic deformation before fracture. The stress-strain curve shows:

  • A clear linear region followed by a yield point
  • A long plastic region where the material "necks" (cross-section reduces locally)
  • Fracture occurs after considerable elongation (strain > 10% for many metals)

Definition. Ductile behaviour is the ability of a material to undergo large plastic deformation before fracture.

Brittle Materials (e.g., Glass, Ceramics)

A brittle material fractures with little or no plastic deformation. The stress-strain curve shows:

  • A linear region right up to fracture
  • No yield point, no plastic region
  • Fracture at relatively low strain (typically < 1%)

Definition. Brittle fracture is the sudden failure of a material with little or no plastic deformation. It occurs when cracks propagate rapidly through the material.

Polymeric Materials (e.g., Rubber, Polyethylene)

Polymers show a wide range of behaviours:

  • Rubber: very large elastic strains (up to 500%), low Young's modulus, returns to original shape. The stress-strain curve is non-linear (S-shaped).
  • Polyethylene: initial elastic region followed by yielding and plastic deformation. Can undergo cold drawing (necking and drawing of the neck along the sample).
  • Thermoplastic polymers: soften when heated, can be remoulded. Show viscoelastic behaviour (time-dependent response).
info

info and requires interpretation of force-extension graphs. Edexcel asks for quantitative analysis of stress-strain graphs including calculating the area under the graph (energy). CIE may ask you to sketch stress-strain curves for different material types and identify specific points. OCR (A) links material properties to engineering applications.

5. Elastic Potential Energy

Definition. Elastic potential energy (or elastic strain energy) is the energy stored in a deformed elastic body.

Energy in a Spring

From Hooke's law, the force varies linearly from 00 to FF as the spring extends from 00 to Δx\Delta x. The energy stored equals the area under the force-extension graph:

Ee=12FΔx=12kΔx2\boxed{E_e = \frac{1}{2}F\,\Delta x = \frac{1}{2}k\,\Delta x^2}

Proof of Energy Stored in a Wire

Consider a wire of original length LL and cross-sectional area AA. When stretched by an increment d(ΔL)d(\Delta L), the work done is:

dW=Fd(ΔL)dW = F\,d(\Delta L)

Since F=σAF = \sigma A and σ=Eε=EΔL/L\sigma = E\varepsilon = E\,\Delta L/L:

dW=σAd(ΔL)=EεALdε=EALεdεdW = \sigma A\,d(\Delta L) = E\varepsilon A \cdot L\,d\varepsilon = EAL\,\varepsilon\,d\varepsilon

Integrating from ε=0\varepsilon = 0 to ε=εmax\varepsilon = \varepsilon_{\max}:

Ee=0εmaxEALεdε=EAL[LBε2RB◆◆LB2RB]0εmax=12EALεmax2E_e = \int_0^{\varepsilon_{\max}} EAL\,\varepsilon\,d\varepsilon = EAL\left[\frac◆LB◆\varepsilon^2◆RB◆◆LB◆2◆RB◆\right]_0^{\varepsilon_{\max}} = \frac{1}{2}EAL\,\varepsilon_{\max}^2

Since Eε=σE\varepsilon = \sigma and AL=VAL = V (volume of the wire):

Ee=12LBσ2RB◆◆LBERBV\boxed{E_e = \frac{1}{2}\,\frac◆LB◆\sigma^2◆RB◆◆LB◆E◆RB◆\,V}

Alternatively, using ε=σ/E\varepsilon = \sigma/E:

Ee=12EVε2=12σεVE_e = \frac{1}{2}\,E\,V\,\varepsilon^2 = \frac{1}{2}\,\sigma\,\varepsilon\,V

\square

warning

warning (Hookean)** region. If the material has been loaded beyond the limit of proportionality, the energy stored is the area under the actual (non-linear) force-extension curve, which must be found by integration or by counting squares.

6. Material Properties Comparison

Metals

PropertySteelCopperAluminium
EE (GPa)20013070
UTS (MPa)400–2000200–400100–600
DuctilityHighVery highHigh
Density (kg/m³)780089002700
BehaviourDuctile, strongDuctile, malleableDuctile, lightweight
ApplicationsConstruction, toolsWiring, plumbingAircraft, packaging

Metals are ductile because their crystalline structure allows dislocations (defects in the crystal lattice) to move under stress. This is the basis of plastic deformation in metals.

Polymers

PropertyPolyethylene (HDPE)Rubber
EE (GPa)0.2–1.00.01–0.1
UTS (MPa)20–4010–30
Max strain~100% (breaks)~500% (elastic)
BehaviourThermoplastic, stiffensElastomer, highly elastic
ApplicationsBottles, pipesTyres, elastic bands

Polymers consist of long-chain molecules. In rubber, the chains are tangled and uncoiled when stretched — this is why it can undergo large elastic strains. In thermoplastics like polyethylene, the chains can slide past each other, leading to plastic deformation.

Ceramics

PropertyGlassConcrete
EE (GPa)7030
Compressive strength (MPa)100030–50
Tensile strength (MPa)30–903–5
BehaviourBrittleBrittle (in tension)
ApplicationsWindows, opticsBuildings, foundations

Ceramics are strong in compression but weak in tension. This is because their ionic/covalent bonding is very strong but cracks propagate easily under tensile stress. Concrete is typically reinforced with steel bars (rebar) to compensate for its low tensile strength.

Composites

Definition. A composite material combines two or more constituent materials with significantly different physical or chemical properties to create a material with characteristics superior to either component alone.

Examples:

  • Fibreglass: glass fibres embedded in a polymer matrix — combines the strength of glass with the toughness of polymers.
  • Carbon fibre reinforced polymer (CFRP): carbon fibres in epoxy resin — extremely high strength-to-weight ratio, used in aircraft and Formula 1.
  • Reinforced concrete: steel bars in concrete — steel provides tensile strength; concrete provides compressive strength and protects steel from corrosion.
  • Wood: a natural composite of cellulose fibres (strong in tension) in a lignin matrix (provides rigidity).

7. Key Definitions Summary

TermDefinition
Young's modulusThe ratio of tensile stress to tensile strain within the limit of proportionality: E=σ/εE = \sigma/\varepsilon
Ultimate tensile strengthThe maximum stress a material can withstand before fracture (necking begins)
Yield stressThe stress at which a material begins to deform plastically
Brittle fractureSudden failure with little or no plastic deformation
Ductile behaviourThe ability to undergo large plastic deformation before fracture
Elastic deformationDeformation from which the material fully recovers when the load is removed
Plastic deformationPermanent deformation that remains after the load is removed
StiffnessResistance to elastic deformation; measured by Young's modulus
ToughnessThe energy absorbed before fracture; area under the full stress-strain curve
HardnessResistance to surface indentation or scratching

8. Loading, Unloading, and Hysteresis

When a material is loaded and then unloaded within the elastic region, the loading and unloading curves coincide — all stored energy is recovered.

When a material is loaded beyond the elastic limit and then unloaded:

  • The unloading curve is parallel to the original linear region (gradient =E= E)
  • The material does not return to its original length — there is a permanent extension
  • The area between the loading and unloading curves represents the energy dissipated (converted to heat due to internal friction)

Hysteresis is the lag between the loading and unloading curves. It is particularly important for rubber and viscoelastic materials. In a rubber band, the energy dissipated per cycle is the area of the hysteresis loop — this is why a stretched rubber band feels warm when released.

9. Fatigue and Creep

Fatigue is the progressive and localised structural damage that occurs when a material is subjected to cyclic loading. Even stresses well below the yield stress can cause failure after millions of cycles. This is critical in aircraft wings, bridges, and engine components.

Creep is the slow, time-dependent deformation of a material under a constant load, especially at elevated temperatures. It is important in power station components, turbine blades, and lead roofing.

info

info AQA focuses more on the core stress-strain behaviour. CIE may include these in application-style questions about engineering materials.

Problems

Details

Problem 1 A spring of spring constant 250250 N m1^{-1} is stretched by 4.04.0 cm. Calculate: (a) the force applied, (b) the elastic potential energy stored.

Answer. (a) F=kΔx=250×0.040=10F = k\Delta x = 250 \times 0.040 = 10 N.

(b) Ee=12kΔx2=12×250×(0.040)2=0.20E_e = \frac{1}{2}k\Delta x^2 = \frac{1}{2} \times 250 \times (0.040)^2 = 0.20 J.

If you get this wrong, revise: Hooke's Law and Elastic Potential Energy

Details

Problem 2 A copper wire of diameter 1.01.0 mm and length 3.03.0 m supports a load of 8080 N. Calculate the stress and the strain, given that Young's modulus for copper is 1.3×10111.3 \times 10^{11} Pa.

Answer. A=π(0.50×103)2=7.85×107A = \pi(0.50 \times 10^{-3})^2 = 7.85 \times 10^{-7} m2^2.

σ=F/A=80/7.85×107=1.02×108\sigma = F/A = 80 / 7.85 \times 10^{-7} = 1.02 \times 10^8 Pa =102= 102 MPa.

ε=σ/E=1.02×108/1.3×1011=7.8×104\varepsilon = \sigma/E = 1.02 \times 10^8 / 1.3 \times 10^{11} = 7.8 \times 10^{-4}.

Extension: ΔL=εL=7.8×104×3.0=2.3×103\Delta L = \varepsilon L = 7.8 \times 10^{-4} \times 3.0 = 2.3 \times 10^{-3} m =2.3= 2.3 mm.

If you get this wrong, revise: Stress and Strain and Young's Modulus

Details

Problem 3 Two identical springs each of spring constant 150150 N m1^{-1} are connected in parallel and support a 1212 kg mass. Find the total extension.

Answer. kparallel=150+150=300k_{\mathrm{parallel}} = 150 + 150 = 300 N m1^{-1}.

F=mg=12×9.81=117.7F = mg = 12 \times 9.81 = 117.7 N.

Δx=F/k=117.7/300=0.392\Delta x = F/k = 117.7/300 = 0.392 m =39.2= 39.2 cm.

If you get this wrong, revise: Springs in Series and Parallel

Details

Problem 4 A steel wire and a rubber cord have the same dimensions and are subjected to the same tensile force. The Young's modulus of steel is 2.0×10112.0 \times 10^{11} Pa and of rubber is 5.0×1065.0 \times 10^6 Pa. Calculate the ratio of their extensions.

Answer. For the same FF, LL, and AA: ΔL=FL/(AE)\Delta L = FL/(AE), so ΔL1/E\Delta L \propto 1/E.

Ratio: LBΔLrubberRB◆◆LBΔLsteelRB=LBEsteelRB◆◆LBErubberRB=LB2.0×1011RB◆◆LB5.0×106RB=4.0×104\frac◆LB◆\Delta L_{\mathrm{rubber}}◆RB◆◆LB◆\Delta L_{\mathrm{steel}}◆RB◆ = \frac◆LB◆E_{\mathrm{steel}}◆RB◆◆LB◆E_{\mathrm{rubber}}◆RB◆ = \frac◆LB◆2.0 \times 10^{11}◆RB◆◆LB◆5.0 \times 10^6◆RB◆ = 4.0 \times 10^4.

The rubber cord extends 40,00040,000 times more than the steel wire under the same load.

If you get this wrong, revise: Young's Modulus

Details

Problem 5 A material has a Young's modulus of 5.05.0 GPa and a breaking stress of 5050 MPa. Calculate the breaking strain.

Answer. ε=σ/E=50×106/5.0×109=0.010=1.0%\varepsilon = \sigma/E = 50 \times 10^6 / 5.0 \times 10^9 = 0.010 = 1.0\%.

If you get this wrong, revise: Young's Modulus

Details

Problem 6 A force-extension graph for a metal wire is linear up to an extension of 0.800.80 mm with a gradient of 2.5×1052.5 \times 10^5 N m1^{-1}. Beyond this point the wire yields and breaks at an extension of 4.04.0 mm under a force of 300300 N. (a) Calculate the energy stored up to the limit of proportionality. (b) Estimate the total energy stored up to fracture.

Answer. (a) Ee=12FΔx=12×(2.5×105×0.80×103)×(0.80×103)=12×200×0.80×103=0.080E_e = \frac{1}{2}F\,\Delta x = \frac{1}{2} \times (2.5 \times 10^5 \times 0.80 \times 10^{-3}) \times (0.80 \times 10^{-3}) = \frac{1}{2} \times 200 \times 0.80 \times 10^{-3} = 0.080 J.

(b) The total energy is the area under the full force-extension curve up to fracture. Approximating as a triangle from the origin to the breaking point: Etotal12×300×4.0×103=0.60E_{\mathrm{total}} \approx \frac{1}{2} \times 300 \times 4.0 \times 10^{-3} = 0.60 J. (A better estimate would account for the non-linear region, but this is a reasonable approximation.)

If you get this wrong, revise: Elastic Potential Energy

Details

Problem 7 Explain why concrete is reinforced with steel bars. Refer to the stress-strain behaviour of each material.

Answer. Concrete is strong in compression but weak in tension (UTS 3\approx 355 MPa in tension). Steel is strong in both tension and compression (UTS 400\approx 40020002000 MPa) and is ductile. In reinforced concrete, the steel bars carry the tensile loads while the concrete carries the compressive loads. The steel's ductility also means the composite structure deforms gradually rather than failing suddenly, giving warning before collapse.

If you get this wrong, revise: Material Properties Comparison

Details

Problem 8 A steel wire of length 2.52.5 m and diameter 0.800.80 mm is stretched by 3.03.0 mm. Calculate the elastic potential energy stored. (Esteel=2.0×1011E_{\mathrm{steel}} = 2.0 \times 10^{11} Pa)

Answer. A=π(0.40×103)2=5.03×107A = \pi(0.40 \times 10^{-3})^2 = 5.03 \times 10^{-7} m2^2. V=AL=5.03×107×2.5=1.26×106V = AL = 5.03 \times 10^{-7} \times 2.5 = 1.26 \times 10^{-6} m3^3.

ε=3.0×103/2.5=1.2×103\varepsilon = 3.0 \times 10^{-3}/2.5 = 1.2 \times 10^{-3}. σ=Eε=2.0×1011×1.2×103=2.4×108\sigma = E\varepsilon = 2.0 \times 10^{11} \times 1.2 \times 10^{-3} = 2.4 \times 10^8 Pa.

Ee=12σεV=12×2.4×108×1.2×103×1.26×106=1.81×104E_e = \frac{1}{2}\sigma\varepsilon V = \frac{1}{2} \times 2.4 \times 10^8 \times 1.2 \times 10^{-3} \times 1.26 \times 10^{-6} = 1.81 \times 10^{-4} J.

If you get this wrong, revise: Proof of Energy Stored in a Wire

Details

Problem 9 Sketch the stress-strain graph for: (a) a brittle material, (b) a ductile material. Label the key features on each graph.

Answer. (a) Brittle: straight line from origin to fracture point (at low strain, < 1%). Label: linear region, breaking point. No plastic region, no yield point.

(b) Ductile: straight line from origin (linear region), then yield point, then curve rises to a peak (UTS), then declines as necking occurs, finally fracture at high strain (10–40%). Label: limit of proportionality, elastic limit, yield point, UTS, necking, fracture.

If you get this wrong, revise: Stress-Strain Graphs

Details

Problem 10 A student measures Young's modulus for a wire and obtains a value 30% higher than the accepted value. Give three possible sources of error, and state whether each would make the result too high or too low.

Answer.

  1. Measuring the diameter too small — if the micrometer reads low, A=πd2/4A = \pi d^2/4 is too small, so E=FL/(AΔL)E = FL/(A\,\Delta L) is too high. (Makes result too high.)

  2. Not accounting for the initial sag or kinks in the wire — some of the measured extension is taken up by straightening the wire rather than elastic stretching, so ΔL\Delta L is overestimated and EE is too low. (Makes result too low.)

  3. Heating of the wire — if the wire heats up during the experiment (due to repeated loading or ambient temperature change), the wire expands, increasing ΔL\Delta L and reducing EE. (Makes result too low.)

If you get this wrong, revise: Measuring Young's Modulus

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tip

tip Ready to test your understanding of Properties of Materials? The diagnostic test contains the hardest questions within the A-Level specification for this topic, each with a full worked solution.

Unit tests probe edge cases and common misconceptions. Integration tests combine Properties of Materials with other physics topics to test synthesis under exam conditions.

See Diagnostic Guide for instructions on self-marking and building a personal test matrix.

danger

danger

  • Confusing stress, strain, and Young's modulus: Stress is force per unit AREA (Pa = N/m squared), not force per unit length. Strain is the ratio of extension to ORIGINAL length (dimensionless), not extension alone. Young's modulus is stress divided by strain (Pa), and describes stiffness, not strength.

  • Using the wrong area in stress calculations: Stress = F/A where A is the cross-sectional area perpendicular to the force. For a wire under tension, use the cross-sectional area of the wire (pi * r squared), NOT the surface area. For a cube under compression, use the area of the face the force acts on.

  • Assuming the elastic limit equals the yield point: The elastic limit is the point beyond which the material will not return to its original shape when the force is removed. The yield point is where it begins to deform plastically. For many materials, these are approximately the same, but for some (like mild steel), there is a small difference.

  • Confusing ultimate tensile strength with breaking stress: Ultimate tensile strength is the MAXIMUM stress the material can withstand (the peak of the stress-strain curve). Breaking stress is where the material actually fractures (which may be lower if the material necks). They are not always the same.