GATE AE 2007 • Q57 MCQ • 2 Marks Flight Mechanics & Space Dynamics

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Climb, Glide, Ceiling & Turn Performance

Question Statement:

V (True air speed) The maximum rate of climb achievable by this airplane at 5 km altitude will be

Options:

  • (A) 1.65 m/s
  • (B) 0.51 m/s
  • (C) 1.43 m/s
  • (D) 3.65 m/s

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2007 Q.57)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (2 Mark, MCQ) - **Topic**: Inlets, Combustors & Nozzles (Combustor Design & Flame Stabilization) - **Organizing Institute**: IIT Kanpur - **Problem Statement**: > V (True air speed) The maximum rate of climb achievable by this airplane at 5 km altitude will be **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Inlets, Combustors & Nozzles** (Combustor Design & Flame Stabilization) 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 **A**. **3. Comprehensive Options Analysis**: - **(A)** *"1.65 m/s"*: ✅ **CORRECT**. - **(B)** *"0.51 m/s"*: ❌ **INCORRECT**. - **(C)** *"1.43 m/s"*: ❌ **INCORRECT**. - **(D)** *"3.65 m/s"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **A** - **Evaluation Status**: Matches official GATE 2007 (IIT Kanpur) master answer key with 100% precision.
← Previous (Q56) All 2007 Questions Next (Q58) →

Related Atmospheric Flight Mechanics Solved Questions

View All Atmospheric Flight Mechanics PYQs →
GATE AE 2026 Q31 NAT • 1M

An aircraft starts gliding in power-off condition at an altitude of 4 km. Given that the maximum lift to drag ratio of the aircraft is 15, the maximum glide range that the aircraft can cover, measured along the ground, is ________ km (rounded off to the nearest integer).
GATE AE 2026 Q62 NAT • 2M

A gas mixture at a pressure of 800 kPa and a density of 5 kg/m3 enters a turbine stage. The temperature of the gas at the nozzle exit and the stage exit are 790 K and 750 K, respectively. Assume the specific heats are constant for the gas mixture in the range of temperatures considered. The specific heat at constant pressure is 0.72 kJ/kg-K and the ratio of specific heats is 1.33. The value of the degree of reaction of the turbine stage is ________ (rounded off to 2 decimal places).
GATE AE 2025 Q23 MCQ • 1M

For a general aviation airplane, which one of the following has a destabilizing effect on its static roll stability?
GATE AE 2025 Q24 MCQ • 1M

A general aviation airplane is flying at an altitude of 5000 m. The indicated airspeed is 250 km/h. Assume that there are no instrument errors and position errors. Neglecting compressibility effects, which one of the following options is FALSE?

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