Aerospace Engineering > GATE 2016 > Nozzle Flow
For a completely subsonic isentropic flow through a convergent nozzle, which of the following statement is TRUE?
A
Pressure at the nozzle exit > back pressure.
B
Pressure at the nozzle exit < back pressure.
C
Pressure at the nozzle exit = back pressure.
D
Pressure at the nozzle exit = total pressure.

Correct : c

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