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Compressors Gas Dynamics and Gas Turbines - Engineering

Q1:

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 super sonic 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

ANS:D - all of the above

Explanation: No answer description is available.