In rocket engine the flow in the throat of the nozzle is __________
A. subsonic
B. laminar
C. turbulent
D. none of the mentioned
Answer:A
In rocket engine the flow in the throat of the nozzle is __________
A. subsonic B. laminar C. turbulent D. none of the mentioned
Explanation: In the throat of nozzle mach number is less than one which indicates the flow is subsonic.[/expand]