Rateau turbine is______________
A) pressure-velocity compounded turbine
B) simple reaction turbine
C) velocity compounded turbine
D) pressure compounded turbine
Correct Answer:
Verified
Q6: In rocket engines the amount of expansion
Q7: De-Laval turbine is a_
A)multi rotor impulse turbine
B)impulse
Q8: The Parsons' reaction turbine has
A)only moving blades
B)only
Q9: What is the critical pressure ratio for
Q10: The ratio of the useful heat drop
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
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