Multiple Choice
In rocket engine the flow in the throat of the nozzle is __________
A) subsonic
B) laminar
C) turbulent
D) none of the mentioned
Correct Answer:

Verified
Correct Answer:
Verified
Related Questions
Q10: Aeroderivative engines are used where _ power
Q11: Gas turbines operate at pressures _ than
Q12: In rocket engines the amount of expansion
Q13: How is air produced in mechanical draught
Q14: Coefficient of contraction is the_<br>A)ratio of actual
Q16: Pressure ratios below 20 are used in
Q17: When mach number is greater than one
Q18: Why is exhaust steam coming out of
Q19: Pressure loss occurs in nozzle due to
Q20: Critical pressure ratio is ratios of pressures