85) A gas turbine used in air-craft should have low weight and small frontal area.
Answer is:
Correct
Related Compressors Gas dynamics and Gas Turbines MCQ with Answers
Answer is:
Agree
Answer is:
all of the above
Explanation:
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
