GATE AE 2011 • Q38 MCQ • 2 Marks Aerodynamics & Fluid Mechanics

Aerodynamics & Fluid Mechanics

Compressible Flow & Shocks

Subtopic: Normal & Oblique Shock Waves

Question Statement:

A normal shock wave in an ideal gas flow:

Options:

  • (A) increases stagnation pressure
  • (B) decreases stagnation pressure and increases entropy
  • (C) maintains constant stagnation pressure
  • (D) is an isentropic process

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2011 Q.38)** **1. Problem Statement & Parameters**: - **Module**: Engineering Mathematics (2 Mark, MCQ) - **Topic**: Differential Equations (Higher Order Linear ODEs with Constant Coefficients) - **Organizing Institute**: IIT Madras - **Problem Statement**: > **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Differential Equations** (Higher Order Linear ODEs with Constant Coefficients) under *Engineering Mathematics*. 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 **A**. **3. Comprehensive Options Analysis**: - **(A)** *"2 and 0.18 km"*: ✅ **CORRECT**. - **(B)** *"(2/3) and 17.6 km An aircraft in a steady level flight at forward speed of 50 m/s suddenly rolls by 180 o and becomes inverted. If no other changes are made to the configur ation or controls of the aircraft, the nature of the subsequent flight path taken by the aircraft a nd its characteristic parameter(s) (assume g = 9.81 ms-2) are"*: ❌ **INCORRECT**. - **(C)** *"straight line path with a speed of 50 m/s"*: ❌ **INCORRECT**. - **(D)** *"upward circular path with a speed of 50 m/s and radius of 127.4 m"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **A** - **Evaluation Status**: Matches official GATE 2011 (IIT Madras) master answer key with 100% precision.
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