Aerospace Engineering > GATE 2021 > Nozzle Flow
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 to be operating in: _______.
A
over-expanded mode and under-expanded mode
B
under-expanded mode and perfectly expanded mode
C
perfectly expanded mode and under-expanded mode
D
under-expanded mode and over-expanded mode

Correct : a

Similar Questions

For a completely subsonic isentropic flow through a convergent nozzle, which of the following statement is TRUE?
#494 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

No tags found

Unique Visitor Count

Total Unique Visitors

Loading......