GATE AE 2026 • Q45 MSQ • 2 Marks Aerospace Structures

Aerospace Structures

Strength of Materials & Elasticity

Subtopic: Stress and Strain Tensors & Generalized Hooke's Law

Question Statement:

The deformation of an open-section bar subjected to pure torsion can be solved by choosing an appropriate Prandtl stress function. Which of the following statements is/are true about the Prandtl stress function?

Options:

  • (A) It satisfies the equilibrium equation
  • (B) It is zero on the lateral surfaces of the bar
  • (C) It satisfies the compatibility equation
  • (D) It does not satisfy the equilibrium equation

Official Answer Key:

A, B, C

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2026 Q.45)** **1. Intuitive Physical Setup & Given Parameters**: The problem concerns the Prandtl stress function $\Phi(x, y)$ used in the formulation of the Saint-Venant torsion of prismatic bars with open or arbitrary cross-sections. We are asked to select all true statements about $\Phi(x, y)$ (MSQ). **2. Step-by-Step Theory of Elasticity Derivation**: 1. **Definition of Prandtl Stress Function**: - For pure torsion of a cylinder with axis along $z$, the only non-zero stress components are shear stresses $\tau_{zx}$ and $\tau_{zy}$. - The Prandtl stress function $\Phi(x, y)$ is defined such that: \tau_{zx} = \frac{\partial \Phi}{\partial y}, \quad \tau_{zy} = -\frac{\partial \Phi}{\partial x} 2. **Equilibrium Equations**: - In the absence of body forces, the 3D equilibrium equations reduce to: \frac{\partial \tau_{zx}}{\partial z} = 0, \quad \frac{\partial \tau_{zy}}{\partial z} = 0 \frac{\partial \tau_{zx}}{\partial x} + \frac{\partial \tau_{zy}}{\partial y} = \frac{\partial}{\partial x}\left(\frac{\partial \Phi}{\partial y}\right) + \frac{\partial}{\partial y}\left(-\frac{\partial \Phi}{\partial x}\right) = \frac{\partial^2 \Phi}{\partial x \partial y} - \frac{\partial^2 \Phi}{\partial y \partial x} = 0 - The equilibrium equation is **identically satisfied** by the definition of $\Phi$. Statement A is **TRUE**, Statement D is **FALSE**. 3. **Compatibility Equation**: - Compatibility of the shear strains gives the governing Poisson equation: \nabla^2 \Phi = \frac{\partial^2 \Phi}{\partial x^2} + \frac{\partial^2 \Phi}{\partial y^2} = -2G\theta where $G$ is shear modulus and $\theta$ is angle of twist per unit length. Statement C is **TRUE**. 4. **Boundary Condition on Lateral Surface**: - The lateral surface of the cylinder is traction-free ($T_i = 0$): \tau_{zx} n_x + \tau_{zy} n_y = 0 \implies \frac{\partial \Phi}{\partial y}\frac{dy}{ds} + \left(-\frac{\partial \Phi}{\partial x}\right)\left(-\frac{dx}{ds}\right) = \frac{d\Phi}{ds} = 0 - Thus, $\Phi$ is constant along the boundary curve. For simply connected cross-sections or open sections, this constant is arbitrarily set to zero: $\Phi = 0$ on the boundary. Statement B is **TRUE**. **3. Comprehensive Options & Distractor Analysis**: - **(A) It satisfies the equilibrium equation**: ✅ **CORRECT**. By definition of stress components via partial derivatives. - **(B) It is zero on the lateral surfaces of the bar**: ✅ **CORRECT**. Required boundary condition for traction-free lateral surface. - **(C) It satisfies the compatibility equation**: ✅ **CORRECT**. Leads to $\nabla^2 \Phi = -2G\theta$. - **(D) It does not satisfy the equilibrium equation**: ❌ **INCORRECT**. Directly contradicts Option A. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **A, B, C** - **Exam Takeaway**: Prandtl's stress function satisfies equilibrium identically, compatibility via $\nabla^2\Phi = -2G\theta$, and traction-free lateral boundaries via $\Phi_{\text{boundary}} = 0$.
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