SF Prep Notes
02 Physics Notes 🕒 Updated 2026-10-02
Page 1
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.
σ = FA = TA   (N/m² or Pascal)
FF acc. = 0 FF TT T = F
  • Cut the rod (in equilibrium) at any section : each part is in equilibrium ⇒ internal tension T = F.

3. Strain (φ)

Strain = change in shape or sizeoriginal shape or size
φ = Δll  (length)  ;  φ = ΔVV  (volume)
  • Strain is a ratio ⇒ unitless & dimensionless.

4. Hooke's Law – Modulus of Elasticity

  • Within the limit of proportionality, stress ∝ strain :
Stress = E × Strain  ⇒  σ = E φ
  • 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).
Tensile stress (pulled) FF l + Δl Compressive stress (pushed) FF l − Δl
  • Assumption : area of cross-section A remains the same.

Stress σ = FA ,   Strain φ = Δll ,   Stress = Y (Strain)

FA = YΔll  ⇒  F = AYl Δl
  • Y → Young's modulus (modulus of elasticity for change in length).
Elongation   Δl = F lA Y

6. Wire as a Spring

  • Wire : F = (AY/l) Δl ;  Spring : F = k x  ⇒ a wire behaves like a spring of constant
k = AYl
  • For the same material : k ∝ A/l ∝ r²/l.

7. Series & Parallel Combination

Series (wires joined end to end) :

k₁k₂
1keq = 1k₁ + 1k₂

Parallel (wires side by side) :

k₁k₂
keq = k₁ + k₂

(use k = AY/l for each wire)

Page 2
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 k x² = ½ AYl(Δl)²

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) :
UVol. = ½ Y(Strain)² = ½ (Stress)(Strain)
UVol. = (Stress)²2Y
  • 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.
Breaking force  Fb = σb A
  • Thicker wire (bigger A) needs a bigger force to break : F₁ = σbA₁ , F₂ = σbA₂.

10. Solved Example – Work in Stretching

Q. Work done in stretching a wire by 1 mm is 2 J. Find the work needed to stretch another wire of the same material, with double the radius and half the length, by 1 mm.
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
Stress = TA  ,  Strain = TAY

Total elongation :

  • Element of length dx stretches by δx :

Strain = δxdx = TAY  ⇒  δx = T dxAY

Δl = ∫ T dxAY

Energy stored :

dU = (Stress)²2Y(Vol.) = (T/A)²2Y(A dx)

U = ∫ T²2AY dx

12. Solved Example – Hanging Rod

Q. A rod of mass m, area A, length l, Young's modulus Y hangs from the roof. Find (1) stress & strain at distance x from the bottom, (2) total elongation, (3) total elastic energy stored.
T = mg dx x T = 0

(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

Δl = mgl2AY

(3) Elastic energy stored :

U = ∫₀l T²2AYdx = m²g²2AYl²∫₀l x² dx = m²g²2AYl² · l³3

U = m²g²l6AY

(Δl is half of what the full weight mg would produce if hung at the end.)

Page 3
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.
a x F₁F₂ m₁ = (m/l)x

Acceleration : a = F₂ − F₁m

Left part (length x) : T − F₁ = m₁a = mlx · F₂ − F₁m

T = F₁ + (F₂ − F₁)l x
Tx F₁F₂ 0l
  • 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]

Δl = (F₁ + F₂) l2AY
  • Both tensile / both compressive → use F₁ + F₂.
  • One tensile, one compressive → use the difference (tensile − compressive).

14. Cases

CaseForcesΔl
Ex 1F pull at both ends(F + F)l/2AY = Fl/AY
Ex 2F pull at one end only (other end free)(F + 0)l/2AY = Fl/2AY
Ex 3F₁ push (comp.), F₂ pull (tensile)(F₂ − F₁)l/2AY
Ex 4F₁ & F₂ both push (comp.)(F₁ + F₂)l/2AY  (decrease)
Ex 5F 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)

10F4F F2F3F llll T₁=10FT₂=9F T₃=7FT₄=4F
  • 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)

length l , radius r FF length l + Δl , radius r − Δr
  • Stretching a wire increases its length but decreases its radius.
μ = − transverse (lateral) strainlongitudinal strain = − Δr / rΔl / l
  • 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).
Page 4
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.
StressStrainO AB CD θ elastic elastic + plastic plastic
PartName / meaning
OAProportional limit : stress ∝ strain (Hooke's law) ; slope of OA = tanθ = E
OBElastic limit : wire returns to its original length after removing the force
BCElastic + plastic : some recovery, but some permanent deformation
CDPlastic : no recovery
BYield point
CUltimate point (ultimate tensile strength)
DFracture point (wire breaks)

18. Brittle & Ductile Materials

StressStrainO Brittle (B ≈ D) B D Ductile
  • 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)

ΔPV V − ΔV
  • Volume stress = change in pressure (ΔP) — equal force per area on all faces.
  • Volume strain = change in volumeoriginal volume = ΔVV
ΔP = − β ΔVV  ⇒  β = − V dPdV
  • 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
Compressibility  K = 1β
Materialβ (Pa)
Air1.01 × 10⁵ (isothermal) to 1.42 × 10⁵ (adiabatic)
Water≈ 2.1 × 10⁹ – 2.2 × 10⁹
Steel1.6 × 10¹¹

Gases are the most compressible, solids the least.

20. Change in Volume & Density with Depth

A (P₀)h B air, P₀ PB = P₀ + ρgh
  • 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
Δρρ = −ΔVV = ΔPβ = ρghβ
Page 5
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.
F∥ F∥ x l φ side view
Shear stress = FA  ,  Shear strain φ ≈ tanφ = xl
FA = η xl  ⇒  η = F / Aφ
  • η → modulus of rigidity (shear modulus) ; φ in radian (small angle).

22. Solved Example – Oblique Section

Q. A rod (area A) is pulled by F at both ends. For a cross-section AB making angle θ with the normal cross-section, find (1) the shear stress and longitudinal (normal) stress on AB, (2) θ for which each is maximum.
θ AB A secθ FF
Fnet = 0 ⇒ acc. = 0 ; force on section AB = F (along the rod).
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

Y = 2η (1 + μ)

(Young's modulus & modulus of rigidity)

Y = 3β (1 − 2μ)

(Young's modulus & bulk modulus)

Y = 9ηβη + 3β   or   9Y = 3η + 1β

(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

QuantityFormula
Stressσ = F/A
Young's modulusY = (F/A)/(Δl/l) ; Δl = Fl/AY
Wire as springk = AY/l
Energy / volume½ Y(strain)² = ½ stress × strain = stress²/2Y
Breaking forceFb = σbA
Variable TΔl = ∫T dx/AY ; U = ∫T² dx/2AY
Hanging rod (own weight)Δl = mgl/2AY ; U = m²g²l/6AY
Rod with F₁, F₂Δl = (F₁ + F₂)l/2AY
Poisson ratioμ = −(Δr/r)/(Δl/l)
Bulk modulusβ = −V dP/dV ; K = 1/β
Density at depthΔρ/ρ = ρgh/β
Shear modulusη = (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.