GATE AE 2026 • Q34 NAT • 1 Mark

Aerospace Structures

Structural Dynamics & Aeroelasticity

Subtopic: Flutter Phenomenon & Divergence Speed

Question Statement:

The vortex shedding frequency behind a landing gear model is found to be 50 Hz when tested in a wind tunnel operating at 5 m/s. If the actual landing gear size is 10 times that of the model, and it is designed to operate at 50 m/s, then the expected vortex shedding frequency behind it is ________ Hz (rounded off to the nearest integer).

Official Answer Key:

50.0

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2026 Q.34)** **1. Intuitive Physical Setup & Given Parameters**: - Wind tunnel model test: - Velocity: $V_m = 5 ext{ m/s}$ - Vortex shedding frequency: $f_m = 50 ext{ Hz}$ - Characteristic dimension: $L_m$ - Prototype landing gear: - Scale factor: $L_p = 10 L_m$ - Operating velocity: $V_p = 50 ext{ m/s}$ - We need to find the expected vortex shedding frequency $f_p$ behind the prototype in Hz. **2. Step-by-Step Fluid Dynamic Derivation**: 1. **Dynamic Similarity & Strouhal Number**: - Vortex shedding in bluff body cross-flow (e.g., von Kármán vortex streets behind landing gear cylinders) is governed by the non-dimensional **Strouhal number**: $St = rac{f L}{V}$ - Under dynamic similarity, the Strouhal number is invariant between model and prototype: $St_m = St_p \implies rac{f_m L_m}{V_m} = rac{f_p L_p}{V_p}$ 2. **Solve for Prototype Frequency $f_p$**: $f_p = f_m \left( rac{V_p}{V_m} ight) \left( rac{L_m}{L_p} ight)$ 3. **Substitute Numerical Values**: - Given $ rac{V_p}{V_m} = rac{50}{5} = 10$ - Given $ rac{L_m}{L_p} = rac{1}{10}$ $f_p = 50 imes 10 imes rac{1}{10} = 50 ext{ Hz}$ **3. Comprehensive Options & Distractor Analysis**: - **Evaluation Criteria**: Numerical Answer Type (NAT). - **Exact Analytical Result**: $f_p = 50 ext{ Hz}$. - **Rounding Requirement**: Nearest integer $\implies \mathbf{50}$. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **50.0** (Acceptable Range: **50 to 50**) - **Exam Takeaway**: When both velocity and geometric scale increase by the identical factor ($10 imes$ speed, $10 imes$ length), their effects on Strouhal frequency precisely cancel out, leaving vortex shedding frequency identical.

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