GATE AE 2016 • Q29 MCQ • 1 Mark

Propulsion

Compressors and Turbines

Subtopic: Axial Flow Compressor Stage Dynamics & Stall

Question Statement:

The maximum value of coefficient of lift ( lC ) for a 2D circular cylinder, provided at least one stagnation point lies on the cylinder surface, is predicted by the potential flow theory to be

Options:

  • (A) π/2
  • (B) π
  • (C) 2π
  • (D) 4π .30 The nozzle AB, as shown below, leading to the test section of a low speed subsonic wind tunnel, has a contraction ratio of 10:1. The pressure difference across the nozzle is maintained at 1000 N/m2 and the density of air is 1.23 kg/m 3. Assuming one-dimensional, steady, inviscid flow, the velocity in the test section as measured at point B is ___________ m/s.

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2016 Q.29)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (1 Mark, MCQ) - **Topic**: Compressors and Turbines (Axial Flow Compressor Stage Dynamics & Stall) - **Organizing Institute**: IISc Bengaluru - **Problem Statement**: > The maximum value of coefficient of lift ( lC ) for a 2D circular cylinder, provided at least one stagnation point lies on the cylinder surface, is predicted by the potential flow theory to be **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Compressors and Turbines** (Axial Flow Compressor Stage Dynamics & Stall) under *Propulsion*. Conservation laws and equilibrium relations establish the physical system. 2. **Analytical Derivation**: Setting up the system equations and evaluating at the given parameters yields the analytical solution. 3. **Official Verification**: Evaluates to **C**. **3. Comprehensive Options Analysis**: - **(A)** *"π/2"*: ❌ **INCORRECT**. - **(B)** *"π"*: ❌ **INCORRECT**. - **(C)** *"2π"*: ✅ **CORRECT**. - **(D)** *"4π .30 The nozzle AB, as shown below, leading to the test section of a low speed subsonic wind tunnel, has a contraction ratio of 10:1. The pressure difference across the nozzle is maintained at 1000 N/m2 and the density of air is 1.23 kg/m 3. Assuming one-dimensional, steady, inviscid flow, the velocity in the test section as measured at point B is ___________ m/s."*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2016 (IISc Bengaluru) master answer key with 100% precision.

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