GATE AE 2026 • Q47 MSQ • 2 Marks

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Drag Polar & Aircraft Performance Equations

Question Statement:

Consider the flow over an oval modeled using the elementary potential flows as shown below. U represents uniform flow velocity and 𝛤 represents circulation around an irrotational line vortex. Which of the following statements is/are TRUE for this model?

Options:

  • (A) Increasing U enlarges the oval
  • (B) Increasing 𝛤 enlarges the oval
  • (C) Interchanging the sense of the two vortices does not alter the oval
  • (D) Moving the vortices too far apart causes the oval to break up

Official Answer Key:

B, D

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2026 Q.47)** **1. Intuitive Physical Setup & Given Parameters**: An oval body (Rankine-like oval) is synthesized in 2D potential flow using elementary flows: - Uniform freestream of velocity $U$. - A vortex pair consisting of two counter-rotating irrotational line vortices of circulation $\pm \Gamma$ separated by distance $2d$. We are asked to identify which statements are **TRUE** regarding this flow model (MSQ). **2. Step-by-Step Potential Flow Derivation**: 1. **Governing Stream Function & Stagnation Points**: - The stream function is obtained by superposing uniform flow and the vortex pair: $\psi = U y + \frac{\Gamma}{2\pi} \ln(r_1) - \frac{\Gamma}{2\pi} \ln(r_2)$ - The closed dividing streamline $\psi = 0$ defines the boundary of the closed oval body. - Stagnation points occur where velocity $\vec{V} = \nabla\phi = 0$. 2. **Effect of Parameter Variations**: - **Increasing Freestream Velocity $U$**: Increasing $U$ compresses the streamlines closer to the vortex centers, shrinking the closed dividing streamline. Statement A is **FALSE**. - **Increasing Circulation $\Gamma$**: Increasing vortex strength $\Gamma$ induces stronger opposing velocities further out, pushing the stagnation points further away and **enlarging the oval**. Statement B is **TRUE**. - **Interchanging Sense of Vortices**: Reversing the signs of $\Gamma$ reverses the induced velocity direction (from opposing freestream to assisting it, or flipping stagnation points), which alters the stagnation streamline and shape. Statement C is **FALSE**. - **Vortex Separation Distance**: If the vortices are moved too far apart, the induced flow between them can no longer maintain a single closed dividing streamline enclosing both vortices; instead, the dividing streamline pinches in and splits into two isolated closed bodies around each individual vortex (the oval breaks up). Statement D is **TRUE**. **3. Comprehensive Options & Distractor Analysis**: - **(A) Increasing U enlarges the oval**: ❌ **INCORRECT**. Higher freestream speed overpowers the induced velocities and shrinks the oval. - **(B) Increasing 𝛤 enlarges the oval**: ✅ **CORRECT**. Stronger vortices extend their influence further into the freestream, expanding the closed dividing streamline. - **(C) Interchanging the sense of the two vortices does not alter the oval**: ❌ **INCORRECT**. Alters the sign of the induced velocities and the resulting stagnation streamline shape. - **(D) Moving the vortices too far apart causes the oval to break up**: ✅ **CORRECT**. Beyond a critical separation distance, the single oval bifurcates into two separate closed bubbles. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **B, D** - **Exam Takeaway**: In superposition of potential flows, singularity strength ($\Gamma, \Lambda$) expands body dimensions, while freestream velocity $U$ compresses them.

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