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.