Discussion :: Compressors, Gas Turbines and Jet Engines
- Which of the following statement is correct relating to rocket engines?
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A.
The combustion chamber in a rocket engine is directly analogous to the reservoir of a supersonic wind tunnel |
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B.
The stagnation conditions exist at the combustion chamber |
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C.
The exit velocities of exhaust gases are much higher than those in jet engine |
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D.
All of the above |
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Answer : Option D
Explanation :
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
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