GATE_AE_2027_MOCK_05_Q44
GATE 2027 Aerospace Engineering All-India Master Mock 05 (High-Yield Comprehensive Grand Finale)
MCQ · 2 Marks
Aerodynamics & Fluid Mechanics • Compressible Flow & Shocks • Rayleigh and Fanno Flow
In 1D Rayleigh flow (constant area duct with heat exchange), the maximum static temperature point on the T-s curve occurs at:
(A) M = 1 / \sqrt{\gamma} (which is subsonic for \gamma = 1.4, M ≈ 0.845)
(B) M = 1.0
(C) M = \sqrt{\gamma}
(D) M = \infty
Answer Key:
A
Step-by-Step Verified Solution
### Solution: On the Rayleigh line in the T-s plane, entropy reaches a maximum at M = 1.0, but static temperature reaches its maximum at M = 1/\sqrt{\gamma} ≈ 0.845 for air. Correct: A.