Aerospace Engineering > GATE 2016 > Nozzle Flow
Consider 1-D, steady, inviscid, compressible flow through a convergent nozzle. The total temperature and total pressure are T0, Po respectively. The flow through the nozzle is choked with a mass flow rate of m˙o If the total temperature is increased to 4To, with total pressure remaining unchanged, then the mass flow rate through the nozzle
A
remains unchanged.
B
becomes half of m˙o.
C
becomes twice of mo
D
becomes four times of m˙o.

Correct : b

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Aerospace Engineering GATE 2016 GATE AE 2016 Q34 compressible flow nozzle choked nozzle mass flow mass flow rate total temperature convergent nozzle flow 1D steady inviscid flow aerodynamics GATE

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