Which of the following statement is correct relating to rocket engines?

A The combustion chamber in a rocket engine is directly analogous to the reservoir of a supersonic wind tunnel
B The stagnation conditions exist at the combustion chamber
C The exit velocities of exhaust gases are much higher than those in jet engine
D All of the above

Correct Answer: All of the above

The combustion chamber in a rocket engine is directly analogous to the reservoir of a supersonic wind tunnel- The stagnation conditions exist at the combustion chamber-The exit velocities of exhaust gases are much higher than those in jet engine
Bissoy MCQ
#Mechanical Engineering #Compressors #Gas Turbines And Jet Engines

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