Discussion :: Compressors,Gas Dynamics and Gas Turbines
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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 super sonic 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 :
No answer description available for this question.
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