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
Q9: A nozzle used to send fluid in
Q10: In fountains the type of nozzle used
Q11: Nozzles used in blast furnaces are called
Q12: If mach number is less than one
Q13: Nozzle used in rocket engine is _
A)convergent
Q15: When mach number is greater than one
Q16: In rocket engines the amount of expansion
Q17: Pressure ratios below 20 are used in
Q18: Aeroderivative engines have pressure ratios _
A)greater than
Q19: Aeroderivative engines are used where _ power
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