GATE AE 2024 • Q21 MCQ • 1 Mark

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Standard Atmosphere Properties

Question Statement:

In the context of steady, inviscid, incompressible flows, consider the superposition of a uniform flow with speed U along the positive x-axis (from left to right), and a source of strength Λ located at the origin. Which one of the following statements is NOT true regarding the location of the stagnation point of the resulting flow?

Options:

  • (A) It is located to the left of the origin
  • (B) It moves closer to the origin for increasing Λ, while U is held constant
  • (C) It moves closer to the origin for increasing U, while Λ is held constant
  • (D) It is located along the x-axis

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2024 Q.21)** **1. Intuitive Physical Setup & Given Parameters**: In 2D potential flow, we consider the superposition of a uniform stream $U_\infty$, a source of strength $\Lambda$, and an equal-strength sink of strength $-\Lambda$ placed at a distance $2a$ apart along the flow axis. **2. Step-by-Step Mathematical Derivation**: 1. **Superposition of Elementary Potential Flows**: The stream function for the combined flow is: $\psi(x, y) = U_\infty y + \frac{\Lambda}{2\pi}\theta_1 - \frac{\Lambda}{2\pi}\theta_2$ where $\theta_1$ and $\theta_2$ are the polar angles from the source at $(-a, 0)$ and sink at $(+a, 0)$. 2. **Dividing Streamline & Body Shape**: The dividing streamline $\psi = 0$ forms an oval-shaped closed streamline that isolates the fluid emitted by the source and absorbed by the sink from the outer streamflow. 3. **Physical Identification**: This closed streamline represents flow over a symmetric elongated body known as a **Rankine oval** (or Rankine body). - If source and sink coalesce ($a \to 0$) keeping $\Lambda \cdot (2a) = \text{const}$, it becomes a **doublet**, yielding flow past a circular cylinder. - A uniform flow plus a single source yields a semi-infinite open body known as a **Rankine half-body**. **3. Comprehensive Options & Distractor Analysis**: - **(A) circular cylinder**: ❌ **INCORRECT**. Flow over a circular cylinder requires uniform flow + doublet (coincident source-sink pair). - **(B) Rankine oval**: ✅ **CORRECT**. A uniform flow combined with a separated source-sink pair forms a closed Rankine oval. - **(C) Rankine half-body**: ❌ **INCORRECT**. A half-body requires uniform flow + single source only. - **(D) vortex sheet**: ❌ **INCORRECT**. Generated by a distribution of point vortices. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **B** - **Exam Takeaway**: Remember the classic potential flow bodies: 1) Uniform + Source = Half-body (open), 2) Uniform + Source + Sink = Rankine oval (closed), 3) Uniform + Doublet = Circular Cylinder (closed).

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