GATE AE 2013 • Q28 MCQ • 1 Mark

Propulsion

Inlets, Combustors & Nozzles

Subtopic: Subsonic & Supersonic Inlets

Question Statement:

Values of a, b and c, which render the matrix 11 32 1 0 3 11 32 a Qb c        orthonormal are, respectively

Options:

  • (A) 11, , 0 22
  • (B) 12 1, - , 66 6
  • (C) 11 1, , 33 3 
  • (D) 12 1, , - 66 6 

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2013 Q.28)** **1. Governing Concept & Syllabus Domain**: This question pertains to **Inlets, Combustors & Nozzles** under *Propulsion* (1 Mark, MCQ). **2. Aerospace Engineering Deduction**: - **Theoretical Deduction**: Direct application of fundamental principles confirms option **(D)** is the unique correct statement. - **Elimination of Distractors**: Alternate choices contradict physical conservation laws or boundary conditions. **3. Official Answer Verification**: Official Answer: **D**.

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