Aerospace Engineering > GATE 2020 > Nozzle Theory
In aircraft engine thermodynamic cycle analysis, perfectly expanded flow in the nozzle means that the static pressure in the flow at the nozzle exit is equal to
A
the stagnation pressure at the engine inlet.
B
the stagnation pressure at the nozzle exit.
C
the ambient pressure at the nozzle exit.
D
the static pressure at the nozzle inlet.

Correct : c

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Related Topics

aerospace thermodynamic cycle engine nozzle analysis GATE Aerospace Engineering 2020 engine thermodynamic cycle perfectly expanded flow stagnation pressure nozzle exit pressure static pressure inlet

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