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problem 1:

Discuss any two fundamental differences between aircraft piston engines and jet engines from operating principle point of view.

problem 2:

Discuss any two advantages and two drawbacks of turbojet powered airplane.

problem 3:

prepare down the effect of increase in air temperature during compression process on the overall jet engine performance.

problem 4:

How do you diminish total pressure loss in design of supersonic inlets.

problem 5:

Make a distinction between primary zone and secondary zone of the gas turbine combustion chamber?

problem 6:

prepare down the function of the swirl vane in the can type gas turbine combustion chamber.

problem 7:

What do you mean by over expanded nozzles?

problem 8:

prepare down the function of impeller in the centrifugal air compressor.

problem 8:

Recommend any two methods to enhance compression efficiency of the axial flow compressor.

problem 9:

Illustrate out the phenomenon ‘surging’ of compressor.

Mechanical Engineering, Engineering

  • Category:- Mechanical Engineering
  • Reference No.:- M912840

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