GATE AE 2024 • Q13 MCQ • 1 Mark Aerospace Structures

Aerospace Structures

Aerospace Materials & Fatigue

Subtopic: Composite Materials & Laminate Theory

Question Statement:

The three-dimensional stress-strain relationship for an isotropic material is given as { $\sigma$xx $\sigma$yy $\sigma$zz $\tau$yz $\tau$xz $\tau$xy} = [ P Q Q Q P Q Q Q P 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 R 0 0 0 R 0 0 0 R] { 𝜀xx 𝜀yy 𝜀zz $\gamma$yz $\gamma$xz $\gamma$xy} where, $P, Q$ and $R$ are the three elastic constants, $\sigma$ and $\tau$ represent normal and shear stresses and 𝜀 and $\gamma$ represent normal and engineering shear strains. Which one of the following options is correct?

Options:

  • (A) $R = \frac{P - Q}{2}$
  • (B) $R = \frac{Q - P}{2}$
  • (C) $Q = \frac{P - R}{2}$
  • (D) $Q = \frac{R - P}{2}$

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2024 Q.13)** **1. Constitutive Relations for Isotropic Linear Elastic Material**: For an isotropic material, Hooke's law relates normal stresses to normal strains and shear stresses to engineering shear strains: $$\sigma_{xx} = P \varepsilon_{xx} + Q \varepsilon_{yy} + Q \varepsilon_{zz}$$ $$\tau_{xy} = R \gamma_{xy}$$ In terms of Lamé constants $\lambda$ and $\mu = G$: $$P = \lambda + 2G, \quad Q = \lambda, \quad R = G$$ **2. Relationship Between $P, Q,$ and $R$**: Subtracting $Q$ from $P$: $$P - Q = (\lambda + 2G) - \lambda = 2G = 2R$$ Dividing by $2$: $$R = \frac{P - Q}{2}$$ **3. Options Analysis**: - **(A) $R = \frac{P - Q}{2}$**: ✅ **CORRECT**. Directly derived from isotropic symmetry relations. - **(B) $R = \frac{Q - P}{2}$**: ❌ **INCORRECT**. Sign error ($P > Q$ for real elastic materials). - **(C) $Q = \frac{P - R}{2}$**: ❌ **INCORRECT**. Violates Lamé identity. - **(D) $Q = \frac{R - P}{2}$**: ❌ **INCORRECT**. **4. Official Master Key**: - **Official Answer Key**: **A** - **Exam Takeaway**: For an isotropic elastic solid, shear modulus $G$ relates Lamé constants by $G = \frac{C_{11} - C_{12}}{2}$. Here $C_{11}=P, C_{12}=Q, G=R \implies R = \frac{P - Q}{2}$.
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