Q10: The ratio of the useful heat drop
Q11: Rateau turbine is_
A)pressure-velocity compounded turbine
B)simple reaction turbine
C)velocity
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.
Q16: Critical pressure ratio is ratios of pressures
Q17: Ratio of critical pressure to inlet pressure
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
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