GATE AE 2025 • Q20 MCQ • 1 Mark

Aerodynamics & Fluid Mechanics

Wind Tunnel Testing & Instrumentation

Subtopic: Pitot-Static Probes & Pressure Transducers

Question Statement:

Consider a pair of point vortices with clockwise circulation Γ each. The distance between their centers is a, as shown in the figure. Assume two-dimensional, incompressible, inviscid flow. Which one of the following options is correct?

Options:

  • (A) The vortices translate downwards together with a velocity Γ 2𝜋a .
  • (B) The vortices translate upwards together with a velocity Γ 2𝜋a .
  • (C) The vortices rotate clockwise around each other about their centroid O.
  • (D) The vortices rotate counter-clockwise around each other about their centroid O.

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2025 Q.20)** **1. Intuitive Physical Setup & Given Parameters**: A pair of 2D point vortices in an inviscid, incompressible fluid: - Both have **identical clockwise circulation** $\Gamma$ (same sign and magnitude). - Distance between their centers: $a$. - Centroid of the two vortices is at point $O$ (midpoint, at distance $a/2$ from each). We need to determine the resulting kinematic motion of the vortex pair. **2. Step-by-Step Potential Flow Derivation**: 1. **Induced Velocity on Each Vortex**: - By the Biot-Savart law in 2D potential flow, a point vortex does not move due to its own velocity field, but is advected by the velocity induced by all other vortices. - Let Vortex 1 be located at $(0, a/2)$ and Vortex 2 at $(0, -a/2)$. - Both have clockwise circulation $\Gamma$. - The velocity induced by Vortex 2 on Vortex 1 is directed perpendicular to the line connecting them: $V_{\text{ind}} = \frac{\Gamma}{2\pi a}$ - Because the circulation is clockwise, the velocity induced at Vortex 1 points to the right. - By symmetry, the velocity induced by Vortex 1 on Vortex 2 has the same magnitude: $V_{\text{ind}} = \frac{\Gamma}{2\pi a}$ but points to the left! 2. **Resulting Motion**: - Because the induced velocity vectors at the two vortex locations are equal in magnitude and point in opposite directions perpendicular to the joining line, the pair undergoes a steady **pure rotation around their midpoint (centroid $O$)**. - Angular velocity: $\Omega = \frac{V_{\text{ind}}}{a/2} = \frac{\frac{\Gamma}{2\pi a}}{a/2} = \frac{\Gamma}{\pi a^2}$ - Tracing the direction of the velocity vectors confirms that the rotation of the pair about $O$ is in the **clockwise** direction. **3. Comprehensive Options & Distractor Analysis**: - **(A) The vortices translate downwards together with a velocity Γ / (2𝜋a)**: ❌ **INCORRECT**. Co-translation occurs for a counter-rotating pair (opposite circulations $\pm \Gamma$), not an identical pair. - **(B) The vortices translate upwards together with a velocity Γ / (2𝜋a)**: ❌ **INCORRECT**. Requires opposite signs of circulation. - **(C) The vortices rotate clockwise around each other about their centroid O**: ✅ **CORRECT**. Identical clockwise circulations induce opposite tangential velocities, rotating the pair clockwise around their midpoint. - **(D) The vortices rotate counter-clockwise around each other about their centroid O**: ❌ **INCORRECT**. Opposite direction of rotation. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **C** - **Exam Takeaway**: Like-sign vortices rotate around their centroid ($\Omega = \Gamma / (\pi a^2)$); opposite-sign vortices translate in a straight line with uniform speed $V = \Gamma / (2\pi a)$.

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