Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines - Discussion

Discussion Forum : Compressors, Gas Dynamics and Gas Turbines - Section 2 (Q.No. 41)

Compressors, Gas Dynamics and Gas Turbines

41.

Which of the following statement is correct relating to rocket engines ?

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

all of the above

Answer: Option

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