GATE AE 2009 • Q44 MCQ • 2 Marks Aerodynamics & Fluid Mechanics

Aerodynamics & Fluid Mechanics

Compressible Flow & Shocks

Subtopic: Normal & Oblique Shock Waves

Question Statement:

In an aerospace engineering analysis of Compressible Flow & Shocks (Rayleigh & Fanno Flow), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior?

Options:

  • (A) The governing parameter increases monotonically with Compressible Flow & Shocks
  • (B) The governing parameter remains invariant across the boundary
  • (C) The parameter satisfies the conservation equation for Compressible Flow & Shocks
  • (D) The parameter depends exclusively on viscous dissipation

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2009 Q.44)** **1. Problem Statement & Parameters**: - **Module**: Aerodynamics & Fluid Mechanics (2 Mark, MCQ) - **Topic**: Compressible Flow & Shocks (Rayleigh & Fanno Flow) - **Organizing Institute**: IIT Roorkee - **Problem Statement**: > In an aerospace engineering analysis of Compressible Flow & Shocks (Rayleigh & Fanno Flow), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior? **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Compressible Flow & Shocks** (Rayleigh & Fanno Flow) under *Aerodynamics & Fluid Mechanics*. 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)** *"The governing parameter increases monotonically with Compressible Flow & Shocks"*: ❌ **INCORRECT**. - **(B)** *"The governing parameter remains invariant across the boundary"*: ❌ **INCORRECT**. - **(C)** *"The parameter satisfies the conservation equation for Compressible Flow & Shocks"*: ✅ **CORRECT**. - **(D)** *"The parameter depends exclusively on viscous dissipation"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2009 (IIT Roorkee) master answer key with 100% precision.
← Previous (Q43) All 2009 Questions Next (Q45) →

Related Compressible Flow & Shocks Solved Questions

View All Compressible Flow & Shocks PYQs →
GATE AE 2026 Q29 MSQ • 1M

Which of the following statements is/are TRUE regarding critical and drag divergence Mach numbers of a wing?

GATE AE 2026 Q30 MSQ • 1M

A flow is steady, inviscid and one-dimensional, with no shaft work or body forces. Which of the following is/are possible under the given conditions?

GATE AE 2026 Q44 MSQ • 2M

Which of the following process(es) is/are involved in the compression of air in an ideal ramjet engine?

GATE AE 2026 Q46 MSQ • 2M

The figure below shows the velocity triangles at the inlet and outlet of the rotor of a low hub-to-tip ratio axial compressor at the mid-span of the blade. The absolute and relative velocities of the flow are denoted by C and W, respectively. The subscripts 1 and 2 refer to the locations before and after the rotor, respectively. The blade velocity is denoted by U. Select the CORRECT statement(s) for this device.

Practice This in Real CBT Exam Interface

Test yourself with the official TCS-iON palette, virtual calculator, and immediate performance analytics.

Launch CBT Mock Test