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Stress-Strain Curve: Diagram, Zones, Formulae, and Engineering Significance

What is a Stress-Strain Curve?

A stress-strain curve is a graphical representation of a material’s mechanical behaviour when subjected to an axial load. It shows how a material deforms (strain) under applied force (stress) from the elastic region through to fracture.

Definitions

Engineering Stress: σ = F / A₀ (applied force divided by original cross-sectional area, in MPa or N/mm²)

Engineering Strain: ε = ΔL / L₀ (change in length divided by original gauge length, dimensionless or %)

Key Points on the Stress-Strain Curve (Mild Steel)

Point/Zone Description Significance
Proportional Limit (A) Stress proportional to strain (Hooke’s Law) Upper limit of elastic Hooke’s Law behaviour
Elastic Limit (B) Maximum stress with no permanent deformation Material returns to original shape below this
Upper Yield Point (C) Sudden drop in load; crystal structure dislocations move Specific to mild steel and annealed metals
Lower Yield Point (D) Sustained yielding at nearly constant stress Design yield stress often taken here
Ultimate Tensile Strength (E) Maximum stress on the curve; necking begins Maximum load-bearing capacity
Fracture Point (F) Material breaks Ductility and toughness assessed here

Young’s Modulus (E)

In the elastic (proportional) region: E = σ / ε = Stress / Strain

Young’s modulus for common materials:

  • Mild Steel: 200–210 GPa
  • Aluminium: 70 GPa
  • Copper: 110–130 GPa
  • Cast Iron: 100–170 GPa

Percentage Elongation and Reduction in Area

% Elongation = (L_f – L₀) / L₀ × 100 — measures ductility

% Reduction in Area = (A₀ – A_f) / A₀ × 100 — measures ductility at the neck

Brittle vs Ductile Materials

Ductile materials (mild steel, aluminium): large plastic zone, significant necking before fracture, high energy absorption. % elongation > 5%.

Brittle materials (cast iron, glass): little or no plastic zone, fracture near UTS with minimal necking. % elongation < 2%.

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Universal Testing Machine (UTM) Experiment

The stress-strain curve is plotted experimentally using a Universal Testing Machine (UTM). The procedure:

  1. Prepare the specimen per IS:1608 (gauge length = 5.65√A₀ for circular specimens)
  2. Mount the specimen in the UTM grips
  3. Apply tensile load at a controlled crosshead speed (typically 2 mm/min)
  4. Record load vs extension using a load cell and extensometer
  5. Plot stress-strain from the load-extension data
  6. Identify proportional limit, yield point, UTS, and fracture point

Scientico India’s UTM (capacity 40–100 kN) includes data acquisition software to automatically plot the stress-strain curve. Request specifications.

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  • Creep Testing Machine Experiment — Procedure, Creep Curve and Analysis
  • Stress-Strain Curve — Material-by-Material Comparison

    Low Carbon (Mild) Steel — The Classical Stress-Strain Curve

    Mild steel shows all the characteristic zones of a ductile material most clearly:

    • Proportional limit: ~250 MPa — end of linear elastic region (Hooke’s law)
    • Elastic limit: Slightly above proportional limit
    • Upper yield point: ~280 MPa — sudden drop in load (Lüders band formation)
    • Lower yield point: ~240 MPa — plastic flow at near-constant stress
    • Ultimate tensile strength: ~420 MPa — maximum engineering stress
    • Fracture stress: ~350 MPa (engineering) — lower due to neck formation
    • % Elongation: 30–40%

    High Carbon Steel

    No distinct yield point. Higher UTS (700–2000 MPa depending on grade) but lower ductility (elongation 5–15%). Fracture is more sudden.

    Cast Iron (Brittle Material)

    The stress-strain curve for cast iron is nearly linear until fracture — no plastic deformation zone, no yield point, and very low elongation (<1%). Fracture occurs at relatively low stress (100–400 MPa in tension) but cast iron is much stronger in compression (3–5× stronger than in tension).

    Rubber and Polymers (Non-linear Elastic)

    Rubber shows a highly non-linear stress-strain curve — initially soft (low modulus), stiffening at large strains. Young’s modulus is extremely low (0.01–0.1 GPa). Elongation at break can exceed 500%.

    Young’s Modulus Values — Reference Table

    Material E (GPa) UTS (MPa) Elongation (%)
    Mild Steel 200–210 400–550 30–40
    High Carbon Steel 200–210 700–2000 5–15
    Aluminium Alloy 69–72 200–700 10–20
    Copper 110–130 200–400 30–50
    Cast Iron (grey) 100–170 100–400 <1
    Nylon 6,6 2.5–3.5 60–80 20–60

    True Stress vs. Engineering Stress

    Engineering stress: σ_eng = F/A₀ (using original area)

    True stress: σ_true = F/A_instantaneous = σ_eng(1 + ε_eng)

    The true stress curve continues to rise after the UTS (because necking reduces area faster than load drops), while the engineering curve shows a downward slope after UTS.

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