Subsonic Isentropic Flow in Convergent Nozzle: Exit Pressure | GATE AE 2016 Question - Examprev

```

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

Similar Questions

The figure shows schematics of wave patterns at the exit of nozzles A and B operating at different pressure ratios. Nozzles A and B, respectively, are said...

#217 MCQ

Consider 1-D, steady, inviscid, compressible flow through a convergent nozzle. The total temperature and total pressure are T0, Po respectively. The flow throug...

#522 MCQ

The stagnation pressure and stagnation temperature inside the combustion chamber of a liquidrocket engine are 1.5 MPa and 2500 K respectively. The burned gases...

#905 MCQ

Related Topics

subsonic isentropic flow convergent nozzle nozzle exit pressure back pressure Aerospace Engineering GATE 2016 GATE AE 2016 Q6 fluid dynamics nozzle nozzle flow conditions

Unique Visitor Count

Total Unique Visitors

Loading......