GATE AE 2019 • Q59 NAT • 2 Marks Flight Mechanics & Space Dynamics

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Climb, Glide, Ceiling & Turn Performance

Question Statement:

As shown in the figure, a rigid slab CD of weight $W$ (distributed uniformly along its length) is hung from a ceiling using three vertical cables of identical length and cross-sectional area. The central cable is made of steel (Young's modulus = $3E$) and the other two outer cables are made of aluminium (Young's modulus = $E$). The percentage of the total weight taken by the central cable is _________ % (round off to the nearest integer).

Official Answer Key:

60.0

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2019 Q.59 / AE Q.49)** **1. Intuitive Physical Setup & Given Parameters**: - Rigid slab CD: does not bend (remains completely horizontal during displacement). - Three vertical cables of equal length $L$ and equal cross-sectional area $A$. - Two outer cables: made of aluminium with modulus $E_1 = E_3 = E$. - Central cable: made of steel with modulus $E_2 = 3E$. - Total downward weight: $W$. **2. Step-by-Step Structural Mechanics Derivation**: 1. **Geometric Compatibility Condition**: Because the slab is rigid and symmetric, it translates downward by a uniform vertical displacement $\delta$: \delta_1 = \delta_2 = \delta_3 = \delta 2. **Force-Displacement Relations**: Elongation of an axial member under tension $T_i$ is $\delta_i = \frac{T_i L}{A_i E_i}$. Since length $L$ and area $A$ are identical: T_i = \left( \frac{A E_i}{L} \right) \delta = k_i \delta - For outer cables (1 and 3): $T_1 = T_3 = \left(\frac{A E}{L}\right) \delta = k \delta$ - For central cable (2): $T_2 = \left(\frac{A (3E)}{L}\right) \delta = 3k \delta = 3 T_1$ 3. **Static Equilibrium**: Sum of vertical forces: T_1 + T_2 + T_3 = W T_1 + 3T_1 + T_1 = W \implies 5T_1 = W \implies T_1 = \frac{W}{5} 4. **Load Taken by Central Cable ($T_2$)**: T_2 = 3 T_1 = 3 \left(\frac{W}{5}\right) = \frac{3}{5} W = 0.60 W 5. **Percentage of Total Weight**: \text{Percentage} = \frac{T_2}{W} \times 100\% = 60\% **3. Comprehensive Options & Distractor Analysis**: - **Question Type**: Numerical Answer Type (NAT). - **Exact Analytical Result**: **60%** (Acceptable Range: [60, 60]). **4. Official Master Key & Exam Takeaway**: - **Official Answer**: **60.0** - **Exam Rule**: In parallel indeterminate systems with identical deflection: load carried is directly proportional to axial stiffness $AE$ ($T_i \propto E_i$).
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