Hooke's Law & Elastic Constants

Hooke’s law states that within the proportional limit, stress is proportional to strain:
σ=Eε\sigma=E\varepsilon
and
τ=Gγ\tau=G\gamma
. The elastic constants EE, GG, KK, and ν\nu are related by
E=2G(1+ν)=3K(12ν)E=2G(1+\nu)=3K(1-2\nu)
(RK Bansal / GATE SOM).

Key formulas & points

Skim these first — then read the full notes below.

  • Uniaxial Hooke: σ=Eε\sigma=E\varepsilon, δ=PLAE\delta=\dfrac{PL}{AE}.
  • Shear Hooke: τ=Gγ\tau=G\gamma; GG = modulus of rigidity (shear modulus).
  • Bulk modulus: K=pεvK=-\dfrac{p}{\varepsilon_v} (hydrostatic pressure vs volumetric strain).
  • Poisson: ν=εlat/εlong\nu=-\varepsilon_{\mathrm{lat}}/\varepsilon_{\mathrm{long}}.
  • Interrelations: E=2G(1+ν)E=2G(1+\nu), E=3K(12ν)E=3K(1-2\nu), E=9KG3K+GE=\dfrac{9KG}{3K+G}.
  • Generalised Hooke (3-D isotropic): εx=1E[σxν(σy+σz)]\varepsilon_x=\dfrac{1}{E}[\sigma_x-\nu(\sigma_y+\sigma_z)].
  • Only two independent elastic constants for isotropic linear elasticity.

Topic details

Definition and physical meaning

Hooke’s law (uniaxial): within the proportional limit, normal stress is linearly proportional to normal strain:
σ=EεE=σε\sigma=E\varepsilon\qquad\Rightarrow\qquad E=\frac{\sigma}{\varepsilon}

EE is Young’s modulus (modulus of elasticity) — slope of the initial straight portion of the σ\sigmaε\varepsilon curve.
Shear form:
τ=GγG=τγ\tau=G\gamma\qquad\Rightarrow\qquad G=\frac{\tau}{\gamma}

GG is the modulus of rigidity (shear modulus).
Bulk form (hydrostatic pressure p=σhp=-\sigma_h):
K=pΔV/V=pεvK=-\frac{p}{\Delta V/V}=-\frac{p}{\varepsilon_v}
Physical parameters
Symbol
Meaning
SI unit
EE
Young’s modulus
Pa\mathrm{Pa} (often GPa)
GG
Shear modulus
Pa\mathrm{Pa}
KK
Bulk modulus
Pa\mathrm{Pa}
ν\nu
Poisson’s ratio
σ\sigma, τ\tau
Normal / shear stress
Pa\mathrm{Pa}
ε\varepsilon, γ\gamma
Normal / shear strain
εv\varepsilon_v
Volumetric strain
Typical values (steel): E200GPaE\approx 200\,\mathrm{GPa}, G80GPaG\approx 80\,\mathrm{GPa}, ν0.3\nu\approx 0.3, K140K\approx 140160GPa160\,\mathrm{GPa}.

Fig 1.3 — Blue: ductile (mild steel). Red: brittle (cast iron). Ductile: large plastic strain. Brittle: fracture near σᵤ with minimal elongation. % elongation and cup-cone fracture distinguish ductile break in lab tests.

Schematic diagram for study — aligned with standard B.Tech / GATE syllabus.

Comparison of ductile and brittle stress–strain curves. Ductile materials absorb more energy and show warning before fracture; brittle materials fail suddenly.

Core assumptions (state these in exams)

1. Linear elastic behaviour — stress ∝ strain (proportional limit not exceeded).
2. Isotropic material — same EE, GG, ν\nu in all directions.
3. Homogeneous continuum.
4. Small strains — geometry linearised; superposition valid.
5. Isothermal (or constants measured at the working temperature).
6. No time-dependent effects (creep/relaxation neglected).
If the material is anisotropic (composites, wood), a stiffness matrix with more independent constants is required — elementary Hooke formulas do not apply directly.

Derivation summary — elongation of a prismatic bar

Consider a uniform bar of length LL, area AA, under axial load PP.
σ=PA,ε=δL\sigma=\frac{P}{A},\qquad\varepsilon=\frac{\delta}{L}

Hooke: σ=Eε\sigma=E\varepsilon
PA=EδLδ=PLAE\frac{P}{A}=E\frac{\delta}{L}\qquad\Rightarrow\qquad\delta=\frac{PL}{AE}
Strain energy (elastic, gradually applied load):
U=12Pδ=P2L2AE=σ22E(AL)U=\frac{1}{2}P\delta=\frac{P^2 L}{2AE}=\frac{\sigma^2}{2E}\cdot(AL)

Resilience (strain energy density)
u=σ2/(2E)u=\sigma^2/(2E)
; proof resilience uses σy\sigma_y.

Relations among E, G, K, and ν

For an isotropic linear elastic solid, only two constants are independent. Standard identities:

Formulas (Indian textbook notation)

  • E=2G(1+ν)E=2G(1+\nu)
  • E=3K(12ν)E=3K(1-2\nu)
  • E=9KG3K+GE=\frac{9KG}{3K+G}
  • ν=3K2G2(3K+G)\nu=\frac{3K-2G}{2(3K+G)}
  • G=E2(1+ν),K=E3(12ν)G=\frac{E}{2(1+\nu)},\qquad K=\frac{E}{3(1-2\nu)}
Derivation sketch of E=2G(1+ν)E=2G(1+\nu): pure shear is equivalent to equal tension and compression at 4545^\circ. Relating shear strain γ\gamma to principal strains and using τ=Gγ\tau=G\gamma with σ=Eε\sigma=E\varepsilon yields the identity.
Exam tip: Given any two of {E,G,K,ν}\{E,G,K,\nu\}, compute the rest. Check ν<0.5\nu<0.5 so that K>0K>0.

Generalised Hooke’s law (3-D)

For principal (or Cartesian) stresses on an isotropic body:
εx=1E[σxν(σy+σz)]\varepsilon_x=\frac{1}{E}\big[\sigma_x-\nu(\sigma_y+\sigma_z)\big]

εy=1E[σyν(σz+σx)]\varepsilon_y=\frac{1}{E}\big[\sigma_y-\nu(\sigma_z+\sigma_x)\big]

εz=1E[σzν(σx+σy)]\varepsilon_z=\frac{1}{E}\big[\sigma_z-\nu(\sigma_x+\sigma_y)\big]
Shear strains decouple:
γxy=τxyG,γyz=τyzG,γzx=τzxG\gamma_{xy}=\frac{\tau_{xy}}{G},\quad\gamma_{yz}=\frac{\tau_{yz}}{G},\quad\gamma_{zx}=\frac{\tau_{zx}}{G}
Volumetric strain:
εv=εx+εy+εz=12νE(σx+σy+σz)=3(12ν)Eσmean\varepsilon_v=\varepsilon_x+\varepsilon_y+\varepsilon_z=\frac{1-2\nu}{E}(\sigma_x+\sigma_y+\sigma_z)=\frac{3(1-2\nu)}{E}\sigma_{\mathrm{mean}}

with σmean=(σx+σy+σz)/3\sigma_{\mathrm{mean}}=(\sigma_x+\sigma_y+\sigma_z)/3.

Step-by-step problem approach

1. Confirm loading is within the elastic range (or problem states elastic constants apply).
2. Identify known constants; pick the relation that solves for the unknown directly.
3. For δ\delta: use δ=PL/(AE)\delta=PL/(AE) with consistent units.
4. For 3-D stress: write generalised Hooke component-wise; sum for εv\varepsilon_v if needed.
5. Convert GPa ↔ MPa ↔ Pa carefully (1GPa=103MPa=109Pa1\,\mathrm{GPa}=10^3\,\mathrm{MPa}=10^9\,\mathrm{Pa}).
6. Sanity-check: GE/2.6G\approx E/2.6 for ν0.3\nu\approx 0.3; KK should exceed E3\frac{E}{3}.

Common mistakes in exams

• Using E=2G(1ν)E=2G(1-\nu) instead of E=2G(1+ν)E=2G(1+\nu).
• Forgetting that ν\nu is dimensionless while mixing EE in GPa with σ\sigma in MPa.
• Applying δ=PL/AE\delta=PL/AE beyond the elastic limit.
• Using K=E/[3(1+ν)]K=E/[3(1+\nu)] (wrong sign/factor) instead of 3(12ν)3(1-2\nu).
• Treating EE and GG as independent for isotropic materials when a third constant is also freely chosen (over-constrained).
• Confusing modulus of rigidity GG with bulk modulus KK.

Worked examples

Try the problem first — open the solution when you are ready to check.

Find G and K from E and ν

Problem

For steel, E=210GPaE=210\,\mathrm{GPa} and ν=0.3\nu=0.3. Find GG and KK.

Solution

Formulas (Indian textbook notation)

  • G=E2(1+ν)=2102(1.3)=2102.6=80.77GPaG=\frac{E}{2(1+\nu)}=\frac{210}{2(1.3)}=\frac{210}{2.6}=80.77\,\mathrm{GPa}

Formulas (Indian textbook notation)

  • K=E3(12ν)=2103(10.6)=2103×0.4=2101.2=175GPaK=\frac{E}{3(1-2\nu)}=\frac{210}{3(1-0.6)}=\frac{210}{3\times 0.4}=\frac{210}{1.2}=175\,\mathrm{GPa}
Check:
E=2G(1+ν)=2×80.77×1.3210GPaE=2G(1+\nu)=2\times 80.77\times 1.3\approx 210\,\mathrm{GPa}
.

Elongation using Hooke’s law

Problem

A brass bar (E=100GPaE=100\,\mathrm{GPa}) has A=500mm2A=500\,\mathrm{mm^2}, L=2mL=2\,\mathrm{m}, and axial load P=50kNP=50\,\mathrm{kN}. Find δ\delta and strain energy UU.

Volumetric strain under hydrostatic pressure

Problem

A solid copper sphere has K=140GPaK=140\,\mathrm{GPa}. It is subjected to hydrostatic pressure p=70MPap=70\,\mathrm{MPa}. Find volumetric strain and percentage change in volume.

Practice questions

Most-asked interview and GATE questions for this topic — expand any item for a model answer.

  1. 1
    State Hooke’s law for uniaxial loading and name the constant of proportionality.

    Model answer

    Within the proportional limit, stress is proportional to strain: σ=Eε\sigma=E\varepsilon. The constant EE is Young’s modulus (modulus of elasticity).
  2. 2
    Write Hooke’s law in shear form.

    Model answer

    τ=Gγ\tau=G\gamma where GG is the modulus of rigidity (shear modulus) and γ\gamma is the shear strain (in radians).
  3. 3
    What is the generalized Hooke’s law for a 3-D isotropic linear elastic solid?

    Model answer

    εx=1E[σxν(σy+σz)]\varepsilon_x=\dfrac{1}{E}[\sigma_x-\nu(\sigma_y+\sigma_z)] and cyclic for εy,εz\varepsilon_y,\varepsilon_z; shear: γxy=τxy/G\gamma_{xy}=\tau_{xy}/G etc.
  4. 4
    Why does Hooke’s law fail beyond the elastic limit?

    Model answer

    Dislocations and permanent slip make the σ\sigmaε\varepsilon relation nonlinear; unloading does not return to the origin. The material is no longer uniquely described by a single EE.
  5. 5
    How is EE obtained experimentally from a tension test?

    Model answer

    From the initial linear portion of the engineering stress–strain curve: slope E=Δσ/ΔεE=\Delta\sigma/\Delta\varepsilon (secant/tangent in the proportional range).
  6. 6
    Relate EE, GG, and Poisson’s ratio ν\nu.

    Model answer

    E=2G(1+ν)E=2G(1+\nu). Measuring any two of E,G,νE,G,\nu determines the third for isotropic materials.
  7. 7
    What is the difference between elastic limit and proportional limit?

    Model answer

    Proportional limit: end of linearity (σε\sigma\propto\varepsilon). Elastic limit: maximum stress with no permanent set on unloading. They are close for many metals; proportional limit \le elastic limit.
  8. 8
    Express strain energy density for uniaxial Hookean behaviour.

    Model answer

    u=12σε=σ2/(2E)=Eε2/2u=\dfrac{1}{2}\sigma\varepsilon=\sigma^2/(2E)=E\varepsilon^2/2. This is the area under the linear σ\sigmaε\varepsilon line.
  9. 9
    State Hooke’s law for plane stress (σz=0\sigma_z=0).

    Model answer

    εx=(σxνσy)/E\varepsilon_x=(\sigma_x-\nu\sigma_y)/E, εy=(σyνσx)/E\varepsilon_y=(\sigma_y-\nu\sigma_x)/E, εz=ν(σx+σy)/E\varepsilon_z=-\nu(\sigma_x+\sigma_y)/E, γxy=τxy/G\gamma_{xy}=\tau_{xy}/G.
  10. 10
    State Hooke’s law for plane strain (εz=0\varepsilon_z=0).

    Model answer

    σz=ν(σx+σy)\sigma_z=\nu(\sigma_x+\sigma_y) appears. Effective relations use E=E/(1ν2)E'=E/(1-\nu^2) and ν=ν/(1ν)\nu'=\nu/(1-\nu) in 2-D form.
  11. 11
    Can Hooke’s law be written in terms of bulk modulus?

    Model answer

    Yes for hydrostatic loading: p=K(ΔV/V)p=-K(\Delta V/V). Also E=3K(12ν)E=3K(1-2\nu) links EE, KK, and ν\nu.
  12. 12
    What does a nonlinear but elastic material imply for Hooke’s law?

    Model answer

    Stress and strain remain uniquely related and recoverable, but not linear — classical Hooke’s law (σ=Eε\sigma=E\varepsilon) does not hold; a nonlinear constitutive law is needed.
  13. 13
    Why is EE nearly the same in tension and compression for mild steel in the elastic range?

    Model answer

    Atomic bond stiffness is essentially the same for small tension/compression; the initial slope of σ\sigmaε\varepsilon is nearly identical until yielding differs.
  14. 14
    How does temperature typically affect EE for metals?

    Model answer

    Young’s modulus decreases with rising temperature as interatomic forces soften. Design at elevated temperature must use E(T)E(T) from data sheets.
  15. 15
    Write the compliance form: strain in terms of stress for isotropic material (summary).

    Model answer

    Normal strains depend on all three normal stresses via EE and ν\nu; each shear strain depends only on its conjugate shear stress via GG. No coupling between shear and normal for isotropic linear elasticity.

Exams & GATE

  • 1
    Textbook: RK Bansal Ch. 2–3.
  • 2
    Memorise E=2G(1+ν)E=2G(1+\nu) and E=3K(12ν)E=3K(1-2\nu) — extremely frequent GATE numericals.
  • 3
    Units: EE, GG, KK in GPa or MPa; ν\nu is dimensionless.
  • 4
    State “within elastic/proportional limit” in every derivation.

📖 Standard books (India)

  • Strength of MaterialsRK Bansal

    Read: Ch. 2–3

    SOM — beams, torsion, columns, and deflection