Aerospace Engineering > GATE 2023 > Supersonic Flow
Consider a one-dimensional inviscid supersonic flow in a diverging duct with heat addition (Qin) as shown. Which of the following statement(s) is/are always TRUE?
A
Mach number, M2 > M1
B
Stagnation pressure, P1o > P2o
C
Static pressure, P2 > P1
D
Stagnation temperature, T1o < T2o

Correct : a

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Related Topics

Aerospace Engineering GATE 2023 GATE AE 2023 Q44 supersonic flow heat addition diverging duct flow Rayleigh flow gas dynamics stagnation properties Mach number change

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