Elasticity formulas
Master Elasticity through 22 JEE Advanced-level formulas, systematically structured with every variable spelled out. Revise concept-wise, identify the areas where you need improvement, and focus your preparation with greater precision.
Elasticity, every formula
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Stress
Q1NumericalStressA force of $100$ N acts on an area of $2\ \text{m}^2$. The stress is:Longitudinal strain
Q1NumericalStrainA $2$ m wire stretches by $0.004$ m. The strain is (decimal):Hooke's law
within elastic limit
Q1MCQHooke's lawWithin the elastic limit, Hooke's law states:- Astress $\propto$ strain
- Bstress $\propto$ strain$^{2}$
- Cstress = constant
- Dstrain = 0
- A
Young's modulus
Q1MCQYoung's modulusYoung's modulus is:- A$\dfrac{FL}{A\,\Delta L}$
- B$\dfrac{A\,\Delta L}{FL}$
- C$\dfrac{F}{A}$
- D$\dfrac{\Delta L}{L}$
- A
Bulk modulus
Q1MCQBulk modulusThe bulk modulus is:- A$-\dfrac{\Delta P}{\Delta V/V}$
- B$\dfrac{\Delta V/V}{\Delta P}$
- C$\dfrac{F}{A}$
- D$\dfrac{\Delta L}{L}$
- A
Compressibility
Q1MCQCompressibilityCompressibility equals:- A$\dfrac{1}{B}$
- B$B$
- C$B^{2}$
- D$\dfrac{B}{2}$
- A
Shear (rigidity) modulus
Q1MCQShear modulusThe rigidity (shear) modulus is:- A$\dfrac{F/A}{\theta}$
- B$\dfrac{\theta}{F/A}$
- C$\dfrac{FL}{A\,\Delta L}$
- D$\dfrac{\Delta P}{\Delta V/V}$
- A
Poisson's ratio
Q1MCQPoisson's ratioPoisson's ratio is defined as:- A$-\dfrac{\text{lateral strain}}{\text{longitudinal strain}}$
- B$\dfrac{\text{stress}}{\text{strain}}$
- C$\dfrac{F}{A}$
- D$\dfrac{\Delta L}{L}$
- A
Elastic potential energy
Q1MCQElastic PEThe elastic potential energy in a stretched wire is:- A$\tfrac12\times\text{stress}\times\text{strain}\times V$
- B$\text{stress}\times\text{strain}$
- C$\tfrac12 F\Delta L^{2}$
- D$YV$
- A
Energy density
Q1MCQEnergy densityThe elastic energy density is:- A$\tfrac12\dfrac{\text{stress}^{2}}{Y}$
- B$Y\,\text{strain}$
- C$\dfrac{\text{stress}}{Y}$
- D$\dfrac{F}{A}$
- A
Force constant of a wire
Q1MCQForce constantThe force constant of a wire is:- A$\dfrac{YA}{L}$
- B$\dfrac{YL}{A}$
- C$YAL$
- D$\dfrac{L}{YA}$
- A
Extension under load
Q1MCQExtensionThe extension of a wire under load $F$ is:- A$\dfrac{FL}{AY}$
- B$\dfrac{AY}{FL}$
- C$\dfrac{F}{AY}$
- D$FLY$
- A
Thermal stress
Q1MCQThermal stressThe thermal stress in a clamped rod heated by $\Delta T$ is:- A$Y\alpha\Delta T$
- B$\alpha\Delta T$
- C$\dfrac{Y}{\alpha\Delta T}$
- D$Y\Delta T$
- A
Work done in stretching
Q1MCQWork stretchingThe work done in stretching a wire by $\Delta L$ (force $F$) is:- A$\tfrac12 F\Delta L$
- B$F\Delta L$
- C$\tfrac12 F\Delta L^{2}$
- D$2F\Delta L$
- A
Elongation due to own weight
Q1MCQOwn-weight elongationThe elongation of a wire due to its own weight is:- A$\dfrac{\rho g L^{2}}{2Y}$
- B$\dfrac{\rho g L}{Y}$
- C$\dfrac{\rho g L^{2}}{Y}$
- D$\dfrac{\rho g}{2Y}$
- A
Poisson's ratio range
Q1MCQPoisson rangeThe theoretical range of Poisson's ratio is:- A$-1$ to $0.5$
- B$0$ to $1$
- C$-0.5$ to $1$
- D$0$ to $0.5$ only
- A
Volume strain
Q1MCQVolume strainThe volume strain in terms of $\sigma$ and longitudinal strain is:- A$(1-2\sigma)\dfrac{\Delta L}{L}$
- B$(1+2\sigma)\dfrac{\Delta L}{L}$
- C$\sigma\dfrac{\Delta L}{L}$
- D$\dfrac{\Delta L}{L}$
- A
Breaking stress
Q1MCQBreaking stressThe breaking stress of a wire depends on:- Athe material, not the length
- Bthe length only
- Cthe weight only
- Dnothing
- A
Interatomic force constant
r_0 = interatomic spacing
Q1MCQInteratomic constantThe interatomic force constant is:- A$Y r_0$
- B$\dfrac{Y}{r_0}$
- C$Y r_0^{2}$
- D$\dfrac{r_0}{Y}$
- A
Torsion of a wire
Q1MCQTorsionThe restoring torque per unit twist of a wire is:- A$\dfrac{\pi\eta r^{4}}{2L}$
- B$\dfrac{\pi\eta r^{2}}{2L}$
- C$\dfrac{2L}{\pi\eta r^{4}}$
- D$\eta r$
- A
Elastic after-effect
Q1MCQElastic after-effectThe delay in a body returning to its original shape after removing stress is called:- Aelastic after-effect
- Belastic fatigue
- Cplasticity
- Dductility
- A
Stress–strain: elastic limit
Q1MCQElastic limitThe stress beyond which a body does not return to its original shape is the:- Aelastic limit
- Bbreaking stress
- Cyield strain
- Dbulk modulus
- A
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