Supersonic Flow Entropy | GATE 2013 Aerospace Engineering Question 11 | Examprev.com

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Aerospace Engineering > GATE 2013 > Compressible Flow

Which one of the following statements is NOT TRUE for a supersonic flow?

A

Over a gradual expansion, entropy remains constant

B

Over a sharp expansion corner, entropy can increase

C

Over a gradual compression, entropy can remain constant

D

Over a sharp compression corner, entropy increases

Correct : b

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Related Topics

supersonic flow aerospace engineering gate entropy change sharp compression corner sharp expansion corner gradual compression gradual expansion entropy increase gate entropy decrease gate

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