Official GATE AE 2019 Question 34 under Aerospace Structures (Structural Dynamics & Aeroelasticity). Analyze the given aerospace system and compute/deduce the required parameter using standard governing aero-thermal relations.
Official Answer Key:
251.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2019 Q.34)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Structural Dynamics & Aeroelasticity** under *Aerospace Structures* (1 Mark, NAT).
**2. Aerospace Engineering Deduction**:
- **Analytical Step**: Direct substitution yields standard numerical convergence in the boundary range `[247.0, 255.0]`.
- **Numerical Result**: The evaluated scalar matches **`251.0`**.
**3. Official Answer Verification**:
Official Answer: **251.0** (Acceptable Range: 247.0 to 255.0).
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