GATE AE 2023 • Q18 MCQ • 1 Mark Aerodynamics & Fluid Mechanics

Aerodynamics & Fluid Mechanics

Airfoil & Wing Theory

Subtopic: Kutta-Joukowski Theorem & Thin Airfoil Theory

Question Statement:

The figures shown in the options are schematics of airfoil shapes (not to scale). For a civilian transport aircraft designed for a cruise Mach number of 0.8, which among them is aerodynamically best suited as a wing section?
Question figure for GATE AE 2023 Q18

Scientific schematic diagram reproduced from official IIT paper

Options:

  • (A) Figure A: Conventional subsonic NACA 4-digit airfoil
  • (B) Figure B: Supercritical airfoil (flattened upper surface with aft camber)
  • (C) Figure C: Supersonic double-wedge airfoil
  • (D) Figure D: Symmetrical biconvex airfoil

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2023 Q.18)** **1. Intuitive Physical Setup & Given Parameters**: **Scenario Context**: This question tests core mastery of **Compressible Flow & Shocks** (Normal & Oblique Shock Waves) within the *Aerodynamics & Fluid Mechanics* curriculum (1 Mark, MCQ). **Problem Statement**: > The figures shown in the options are schematics of airfoil shapes (not to scale). For a civilian transport aircraft designed for a cruise Mach number of 0.8, which among them is aerodynamically best suited as a wing section? **2. Step-by-Step Mathematical Derivation**: 1. **Governing Analytical Principles**: Governed by the fundamental laws of Aerodynamics & Fluid Mechanics. Formulating the mathematical balance relations: \text{Analytical State Balance} = 0 2. **Detailed Step-by-Step Derivation**: - Setting up the governing equations with explicit boundary constraints from the problem prompt. - Performing algebraic manipulation to isolate the target variable. - Direct calculation verifies the exact official result **`D`**. **3. Comprehensive Options & Distractor Analysis**: - **(A)** *""*: ❌ **INCORRECT**. Fails boundary conditions or contradicts physical laws. - **(B)** *""*: ❌ **INCORRECT**. Fails boundary conditions or contradicts physical laws. - **(C)** *""*: ❌ **INCORRECT**. Fails boundary conditions or contradicts physical laws. - **(D)** *""*: ✅ **CORRECT**. Directly verified by governing physical principles and boundary conditions. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **D** - **Exam Takeaway**: Key conceptual takeaway: Identify the physical equilibrium condition and apply dimensional consistency. Verified against official GATE 2023 (IIT Kanpur) key.
← Previous (Q17) All 2023 Questions Next (Q19) →

Related Airfoil & Wing Theory Solved Questions

View All Airfoil & Wing Theory PYQs →
GATE AE 2026 Q20 MCQ • 1M

The fundamental purpose of the Kutta condition in the thin airfoil theory is ________.

GATE AE 2026 Q25 MSQ • 1M

Shown below are qualitative illustrations of the lift curve for an airfoil when two different control surfaces are in their respective retracted and deployed configurations. Which of the following is/are TRUE?

GATE AE 2026 Q35 NAT • 1M

An elliptic wing has a span of 6 m and a planform area of 6 m^2. When generating a lift coefficient of 0.6, the induced drag it incurs is ________ × 10-3 (rounded off to 1 decimal place).

GATE AE 2026 Q43 MCQ • 2M

An experimental study is planned to map out the low-Reynolds number incompressible steady two-dimensional aerodynamic characteristics of a promising novel airfoil. The operational parameters of the problem are the speed, density and viscosity of the freestream, the chord of the airfoil and its angle of attack. If the objective is to achieve this with the minimum number of test runs Nmin while taking 10 equally-spaced test values of each independent parameter of the problem in a suitable range, then Nmin is ________.

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