Which of the following statement is correct as regard to centrifugal compressors?

The flow of air is parallel to the axis of the compressor.
The static pressure of air in the impeller increases in order to provide centripetal force on the air.
The impeller rotates at high speeds.
The maximum efficiency
✅ The correct answer is option B.

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
✅ The correct answer is option D.