Stress, Strain & Young's Modulus
Mechanical Properties of Solids
1. Elasticity & Plasticity
- Elasticity : ability of a deformed body to return to its original shape and size when the deforming forces are removed.
e.g. rubber band, catapult (slingshot). - Plasticity : inability of a deformed body to return to its original shape and size when the forces are removed.
e.g. putty / clay, crushed can. - Note : Steel wire is more elastic than a rubber band (steel needs a much larger force for the same strain, i.e. larger modulus of elasticity).
2. Stress (σ)
- Stress = internal restoring force per unit area of cross-section between layers of the material.
- Cut the rod (in equilibrium) at any section : each part is in equilibrium ⇒ internal tension T = F.
3. Strain (φ)
- Strain is a ratio ⇒ unitless & dimensionless.
4. Hooke's Law – Modulus of Elasticity
- Within the limit of proportionality, stress ∝ strain :
- E = modulus of elasticity → depends on the material and temperature (not on the size of the body).
- Unit of E : N/m² or Pa (same as stress, since strain has no unit).
- Like a spring : mass m → extension x ; mass 2m → extension 2x.
Effect of temperature :
- As temperature increases, Young's modulus decreases (material becomes easier to stretch).
5. Longitudinal Stress & Strain
- Only change in length is considered (wire or rod).
- Assumption : area of cross-section A remains the same.
Stress σ = FA , Strain φ = Δll , Stress = Y (Strain)
- Y → Young's modulus (modulus of elasticity for change in length).
6. Wire as a Spring
- Wire : F = (AY/l) Δl ; Spring : F = k x ⇒ a wire behaves like a spring of constant
- For the same material : k ∝ A/l ∝ r²/l.
7. Series & Parallel Combination
Series (wires joined end to end) :
Parallel (wires side by side) :
(use k = AY/l for each wire)
Elastic Energy & Variable Tension
8. Elastic Energy Stored in a Wire
- Wire and spring behave alike, so energy stored = work done in stretching :
U = ½ Y (Al)(Δl)²l² = ½ Y (Vol.)(Strain)²
(Volume of wire = A l)
- Energy per unit volume (energy density) — using Stress = Y (Strain) :
- Also U = ½ F Δl (= ½ × load × extension).
9. Breaking Stress & Breaking Force
- Breaking stress σb = minimum stress at which the wire breaks (= maximum stress at which it will not break).
- σb depends only on the material and temperature ⇒ same for all steel wires (at the same temp.), whatever their thickness.
- Thicker wire (bigger A) needs a bigger force to break : F₁ = σbA₁ , F₂ = σbA₂.
10. Solved Example – Work in Stretching
Sol. W = U = ½ k x² = ½ AYl x²
W₁ = ½ AYl(1 mm)² = 2 J
r → 2r ⇒ A → 4A ; l → l/2 ; same Y ⇒ k → 8k
W₂ = ½ (4A)Yl/2(1 mm)² = 8 W₁ = 8 × 2 = 16 J
11. Variable Tension, Stress & Strain
- If the rod is accelerating or has weight, tension T varies along its length : T = T(x).
- Find T by Newton's laws on a part of the rod ; then at that section
Total elongation :
- Element of length dx stretches by δx :
Strain = δxdx = TAY ⇒ δx = T dxAY
Energy stored :
dU = (Stress)²2Y(Vol.) = (T/A)²2Y(A dx)
12. Solved Example – Hanging Rod
(1) Stress & strain at x :
- Tension at x = weight of the part below = mlx · g
T = mgxl , Stress = mgxAl , Strain = mgxAYl
(2) Total elongation :
Δl = ∫₀l T dxAY = mgAYl∫₀l x dx = mgAYl · l²2
(3) Elastic energy stored :
U = ∫₀l T²2AYdx = m²g²2AYl²∫₀l x² dx = m²g²2AYl² · l³3
(Δl is half of what the full weight mg would produce if hung at the end.)
Accelerating Rod & Poisson Ratio
13. Rod Pulled by Two Unequal Forces
- Rod of mass m, length l on a smooth floor ; F₁ (left) and F₂ (right), F₂ > F₁.
Acceleration : a = F₂ − F₁m
Left part (length x) : T − F₁ = m₁a = mlx · F₂ − F₁m
- T varies linearly from F₁ to F₂ ; Stress = T/A, Strain = T/AY.
Total elongation :
Δl = 1AY∫₀l [F₁ + F₂ − F₁lx] dx
= 1AY[F₁l + F₂ − F₁l · l²2]
= lAY[F₁ + F₂ − F₁2]
- Both tensile / both compressive → use F₁ + F₂.
- One tensile, one compressive → use the difference (tensile − compressive).
14. Cases
| Case | Forces | Δl |
|---|---|---|
| Ex 1 | F pull at both ends | (F + F)l/2AY = Fl/AY |
| Ex 2 | F pull at one end only (other end free) | (F + 0)l/2AY = Fl/2AY |
| Ex 3 | F₁ push (comp.), F₂ pull (tensile) | (F₂ − F₁)l/2AY |
| Ex 4 | F₁ & F₂ both push (comp.) | (F₁ + F₂)l/2AY (decrease) |
| Ex 5 | F push at one end, F pull at the other | (F − F)l/2AY = 0 |
(Ex 5 : front half stretched, back half compressed — net change in length is zero.)
15. Composite Rod (Equilibrium)
- Fnet = −10F + F + 2F + 3F + 4F = 0 ⇒ acc. = 0.
- Going left → right : T₁ = 10F, T₂ = 10F − F = 9F, T₃ = 9F − 2F = 7F, T₄ = 7F − 3F = 4F.
- If all parts have the same A and Y : Δl = Σ Til/AY = (10 + 9 + 7 + 4)FlAY = 30Fl/AY.
16. Poisson Ratio (μ)
- Stretching a wire increases its length but decreases its radius.
- Transverse strain = strain along radius ; longitudinal strain = strain along length.
- Range : −1 to +0.5 (theoretical). For most materials 0 < μ < 0.5.
- Negative μ ⇒ material expands sideways when stretched (positive transverse strain with positive longitudinal strain).
Stress–Strain Graph & Bulk Modulus
17. Stress – Strain Graph
- Wire of length l loaded with mass m : Stress = mg/A , Strain = Δl/l. Increase the load and plot.
| Part | Name / meaning |
|---|---|
| OA | Proportional limit : stress ∝ strain (Hooke's law) ; slope of OA = tanθ = E |
| OB | Elastic limit : wire returns to its original length after removing the force |
| BC | Elastic + plastic : some recovery, but some permanent deformation |
| CD | Plastic : no recovery |
| B | Yield point |
| C | Ultimate point (ultimate tensile strength) |
| D | Fracture point (wire breaks) |
18. Brittle & Ductile Materials
- Brittle → very small plastic zone (B to D close) ; breaks soon after the elastic limit (e.g. glass, cast iron).
- Ductile → large plastic zone (B to D far) ; can be drawn into wires (e.g. copper, mild steel).
19. Volume Stress, Strain & Bulk Modulus (β)
- Volume stress = change in pressure (ΔP) — equal force per area on all faces.
- Volume strain = change in volumeoriginal volume = ΔVV
- Negative sign : pressure increase ⇒ volume decreases ; β is positive.
For a gas :
- Isothermal (PV = const) : dPdV = −PV ⇒ β = P
- Adiabatic (PVγ = const) : dPdV = −γPV ⇒ β = γP
| Material | β (Pa) |
|---|---|
| Air | 1.01 × 10⁵ (isothermal) to 1.42 × 10⁵ (adiabatic) |
| Water | ≈ 2.1 × 10⁹ – 2.2 × 10⁹ |
| Steel | 1.6 × 10¹¹ |
Gases are the most compressible, solids the least.
20. Change in Volume & Density with Depth
- At depth h : ΔP = ρgh (ρ = 1000 kg/m³ for water).
- As we go down, water is compressed ⇒ density increases.
- Mass constant : ρV = const ⇒ Δρρ + ΔVV = 0
Shear Modulus & Relations
21. Shear Stress, Strain & Modulus of Rigidity (η)
- Shear stress : sliding (tangential) stress between layers of the material. Force F∥ acts parallel to the top face (area A) ; the bottom face is held fixed.
- η → modulus of rigidity (shear modulus) ; φ in radian (small angle).
22. Solved Example – Oblique Section
Area of AB : A′ = A secθ (for an a × b section : slant length = b secθ ⇒ A′ = a·b secθ).
Components of F : along AB (tangential) = F sinθ ; ⊥ AB (normal) = F cosθ.
(1) Shear stress = F sinθA secθ = FAsinθ cosθ = F2Asin2θ
Longitudinal stress = F cosθA secθ = FAcos²θ
(2) Shear stress is max at θ = 45° (value F/2A) ; longitudinal stress is max at θ = 0° (value F/A).
23. Relation between Y, η, β and μ
(Young's modulus & modulus of rigidity)
(Young's modulus & bulk modulus)
(Y, η and β — obtained by eliminating μ from the two relations above)
- β = bulk modulus, μ = Poisson ratio, η = modulus of rigidity, Y = Young's modulus.
- β > 0 ⇒ 1 − 2μ > 0 ⇒ μ < 0.5 ; η > 0 ⇒ 1 + μ > 0 ⇒ μ > −1. This gives the range −1 < μ < 0.5.
24. Formula Summary
| Quantity | Formula |
|---|---|
| Stress | σ = F/A |
| Young's modulus | Y = (F/A)/(Δl/l) ; Δl = Fl/AY |
| Wire as spring | k = AY/l |
| Energy / volume | ½ Y(strain)² = ½ stress × strain = stress²/2Y |
| Breaking force | Fb = σbA |
| Variable T | Δl = ∫T dx/AY ; U = ∫T² dx/2AY |
| Hanging rod (own weight) | Δl = mgl/2AY ; U = m²g²l/6AY |
| Rod with F₁, F₂ | Δl = (F₁ + F₂)l/2AY |
| Poisson ratio | μ = −(Δr/r)/(Δl/l) |
| Bulk modulus | β = −V dP/dV ; K = 1/β |
| Density at depth | Δρ/ρ = ρgh/β |
| Shear modulus | η = (F/A)/φ , φ ≈ x/l |
Key Points :
- Y, β, η and σb depend only on the material and temperature, not on the dimensions.
- Y decreases as temperature increases.
- For the same material, k = AY/l ∝ r²/l and breaking force ∝ A.
- Isothermal β = P ; adiabatic β = γP.
- Steel is more elastic than rubber (larger Y).
- Within the proportional limit, slope of the stress–strain graph = modulus of elasticity.