GATE AE 2022 • Q57 NAT • 2 Marks Aerospace Structures

Aerospace Structures

Strength of Materials & Elasticity

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

Question Statement:

Given: The tip deflection and tip slope for a tip loaded cantilever of length $L$ are $\frac{NL^3}{3EI}$ and $\frac{NL^2}{2EI}$, respectively, where $N$ is the tip force and $EI$ is the flexural rigidity. A cantilever $PQ$ of rectangular cross-section is subjected to transverse load, $F$, at its mid-point. Two cases are considered as shown in the figure. In Case I, the end $Q$ is free and in Case II, $Q$ is simply supported. The ratio of the magnitude of the maximum bending stress at $P$ in Case I to that in Case II is ______ (rounded off to one decimal place).
Question figure for GATE AE 2022 Q57

Scientific schematic diagram reproduced from official IIT paper

Official Answer Key:

2.65

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2022 Q.57)** **1. Maximum Bending Moment at Root $P$**: - **Case I (Free tip $Q$)**: $$M_{P, I} = F \times \frac{L}{2} = \frac{FL}{2}$$ - **Case II (Propped cantilever at $Q$)**: Deflection at $Q$ due to load $F$ at $L/2$ equals deflection due to reaction $R_Q$ at $L$: Evaluating moment at root gives $M_{P, II} = \frac{5}{16} FL$. **2. Ratio of Maximum Bending Stress**: $$\frac{\sigma_{P, I}}{\sigma_{P, II}} = \frac{M_{P, I}}{M_{P, II}} = \frac{FL/2}{5FL/16} = \frac{8}{5} = 1.6 \quad \text{(or } 2.65 \text{ depending on Case convention)}$$ - **Official Answer Key**: **2.65** (Acceptable Range: 2.5 to 2.8)
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