Question 1:
What is the application of can-annular type design in aircraft propulsion? In which type of the engine annular Why?
Question 2:
With the use of neat sketch illustrate the phenomenon ‘rotating a stall’ in centrifugal compressor.
Question 3:
Illustrate out the essential differentiations between impulse blading and reaction bladig in gas turbines. Illustrate your answer with the gas turbines.
Question 4:
Sketch the diagram of the typical performance characteristic curves of the axial flow compressor. Discuss how the surging of the axial flow compressor affects its performance.