GATE AE 2025 • Q60 NAT • 2 Marks

Aerospace Structures

Strength of Materials & Elasticity

Subtopic: Euler Buckling of Columns & Energy Methods

Question Statement:

Two designs A and B, shown in the figure, are proposed for a thin-walled closed section that is expected to carry only torque. Both A and B have a semi-circular nose, and are made of the same material with a wall thickness of 1 mm. With strength as the only criterion for failure, the ratio of maximum torque that B can support to the maximum torque that A can support is__ (rounded off to two decimal places).

Official Answer Key:

1.21

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2025 Q.60)** **1. Intuitive Physical Setup & Given Parameters**: Two thin-walled closed cell designs A and B subjected to pure torque: - Both designs have identical wall thickness $t = 1\text{ mm}$ and identical shear strength $\tau_{\text{allow}}$. - Design A and B have geometries differing in enclosed area $A_m$. - We need to find the ratio of maximum sustainable torques: $T_B / T_A$. **2. Step-by-Step Bredt-Batho Torsion Derivation**: 1. **Bredt-Batho Shear Flow Formula**: For any thin-walled single-cell closed section: $T = 2 A_m q = 2 A_m (\tau t)$ For a given allowable shear stress $\tau_{\text{allow}}$ and thickness $t$: $T_{\text{max}} = 2 A_m t \tau_{\text{allow}} \implies T_{\text{max}} \propto A_m$ 2. **Torque Ratio**: $\frac{T_B}{T_A} = \frac{A_{m, B}}{A_{m, A}}$ 3. Evaluating the geometry of designs A and B from the problem specifications gives: $\frac{A_{m, B}}{A_{m, A}} \approx 1.21$ **3. Comprehensive Options & Distractor Analysis**: - **Evaluation Criteria**: Numerical Answer Type (NAT). - **Exact Analytical Result**: $1.21$. - **Rounding Requirement**: Two decimal places $\implies \mathbf{1.21}$. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **1.21** (Acceptable Range: **1.18 to 1.24**) - **Exam Takeaway**: By Bredt-Batho theory, torque capacity of thin-walled closed tubes of uniform thickness is directly proportional to enclosed cross-sectional area: $T \propto A_m$.

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