GATE_AE_2027_MOCK_01_Q18
GATE 2027 Aerospace Engineering All-India Master Mock 01 (Foundation & Standard Core Calibration)
MCQ · 1 Mark
Aerodynamics & Fluid Mechanics • Compressible Flow & Shocks • 1D Isentropic Flow & Area-Mach Relations
In a convergent-divergent supersonic nozzle with sonic throat, if the receiver back pressure is lowered below the design exit pressure, the nozzle operates as:
(A) Under-expanded, with expansion fans forming at the nozzle exit lip
(B) Over-expanded, with oblique shock waves forming at the exit
(C) Subsonic diffuser with normal shock in the diverging section
(D) Choked with detached normal shock upstream of the throat
Answer Key:
A
Step-by-Step Verified Solution
### Solution: When back pressure is lower than design exit pressure ($p_b < p_e$), the gas must expand further outside the nozzle, creating Prandtl-Meyer expansion fans at the lip. This is under-expanded. Correct: A.