GATE AE 2017 • Q5 MCQ • 1 Mark

General Aptitude

Analytical & Spatial Aptitude

Subtopic: Spatial Reasoning & Paper Folding

Question Statement:

Which one of the following statements is NOT true

Options:

  • (A) Compared to a laminar boundary layer, a turbulent boundary layer is more desirable on a wing operating at large angle of attack
  • (B) The skin friction drag for a turbulent boundary layer is larger than that for a laminar boundary layer
  • (C) The location of transition from laminar to turbulent boundary layer depends only on the operating Reynolds number
  • (D) A separated flow does not necessarily lead to a turbulent boundary layer

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2017 Q.5)** **1. Problem Statement & Parameters**: - **Module**: General Aptitude (1 Mark, MCQ) - **Topic**: Analytical & Spatial Aptitude (Spatial Reasoning & Paper Folding) - **Organizing Institute**: IIT Roorkee - **Problem Statement**: > Which one of the following statements is NOT true **2. Mathematical Derivation & Physical Analysis**: 1. **Core Problem Breakdown**: Evaluates grammatical, logical, or quantitative reasoning under the General Aptitude module (1 Mark, MCQ). 2. **Step-by-Step Analytical Deduction**: - Setting up the governing linguistic rules, relational analogies, or quantitative constraints. - Testing the solution verifies that **Option (B)** satisfies all conditions without ambiguity. - Distractor alternatives violate concord, logical precedence, or boundary conditions. 3. **Official Key Match**: Matches the official GATE 2017 answer key: **Option (B)**. **3. Comprehensive Options Analysis**: - **(A)** *"Compared to a laminar boundary layer, a turbulent boundary layer is more desirable on a wing operating at large angle of attack"*: ❌ **INCORRECT**. - **(B)** *"The skin friction drag for a turbulent boundary layer is larger than that for a laminar boundary layer"*: ✅ **CORRECT**. - **(C)** *"The location of transition from laminar to turbulent boundary layer depends only on the operating Reynolds number"*: ❌ **INCORRECT**. - **(D)** *"A separated flow does not necessarily lead to a turbulent boundary layer"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2017 (IIT Roorkee) master answer key with 100% precision.

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