In rocket engines the amount of expansion in Nozzle determines the __________
A) exit temperature
B) exit pressure
C) exit temperature & pressure
D) none of the mentioned
Correct Answer:
Verified
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
Q14: In rocket engine the flow in the
Q15: When mach number is greater than one
Q17: Pressure ratios below 20 are used in
Q18: Aeroderivative engines have pressure ratios _
A)greater than
Q19: Aeroderivative engines are used where _ power
Q20: Gas turbines operate at pressures _ than
Q21: Critical pressure ratio is ratios of pressures
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