Increase Mach Number of Supersonic Flow in Duct - GATE 2020 Aerospace Engg Q9 | Examprev

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Aerospace Engineering > GATE 2020 > Compressible Flow

Which of the following options can result in an increase in the Mach number of a supersonic flow in a duct?

A

Increasing the length of the duct

B

Adding heat to the flow

C

Removing heat from the flow

D

Inserting a convergent-divergent section with the same cross-sectional area at its inlet and exit planes

Correct : c

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Related Topics

Mach number supersonic flow Aerospace Engineering GATE 2020 increase Mach number heat addition supersonic flow gas dynamics compressible flow GATE AE 2020 Q9

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