In rocket engine
* The combustion chamber in a rocket engine is directly analogous to the reservoir of a super sonic wind tunnel
* The stagnation conditions exist at the combustion chamber
* The exit velocities of exhaust gases are much higher than those in jet engine
89) Which of the following statement is correct relating to rocket engines ?
Answer is:
all of the above
Explanation:
Related Compressors Gas dynamics and Gas Turbines MCQ with Answers
Answer is:
