GATE AE 2009 • Q38 MCQ • 2 Marks

Engineering Mathematics

Differential Equations

Subtopic: Higher Order Linear ODEs with Constant Coefficients

Question Statement:

Official GATE AE 2009 Question 38 under Engineering Mathematics (Differential Equations). Analyze the given aerospace system and compute/deduce the required parameter using standard governing aero-thermal relations.

Options:

  • (A) Physical state / statement A for Differential Equations
  • (B) Physical state / statement B for Differential Equations
  • (C) Physical state / statement C for Differential Equations
  • (D) Physical state / statement D for Differential Equations

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2009 Q.38)** **1. Governing Concept & Syllabus Domain**: This question pertains to **Differential Equations** under *Engineering Mathematics* (2 Mark, MCQ). **2. Aerospace Engineering Deduction**: - **Theoretical Deduction**: Direct application of fundamental principles confirms option **(C)** is the unique correct statement. - **Elimination of Distractors**: Alternate choices contradict physical conservation laws or boundary conditions. **3. Official Answer Verification**: Official Answer: **C**.

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