Ratio of critical pressure to inlet pressure in known as______________
A) none of the mentioned
B) pressure ratio
C) critical pressure ratio
D) isoentropic pressure ratio
Correct Answer:
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Q12: When the cross-section of a nozzle increases
Q13: Aeroderivative engines have pressure ratios
A)greater than 30
B)lesser
Q14: Aeroderivative engines are larger.
Q15: Aeroderivative engines release higher emissions.
Q16: Critical pressure ratio is ratios of pressures
Q18: In De Laval Nozzle critical pressure ratio
Q19: With the increase in pressure, the exit
Q20: The Prandtl Number approximates
A)momentum diffusivity to thermal
Q21: Pumps increase_
A)pressure
B)velocity
C)momentum
D)heat
Q22: Which among the following is the formula
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