Question 1:
Illustrate out the necessary differentiations in the design of subsonic and supersonic inlets.
Question 2:
What is shock swallowing by area variation in case of supersonic inlet? Illustrate in concept with essential Illustrations.
Question 3:
How is real flow through the jet engine nozzle different form an ideal flow? Discuss at least four essential differences with a brief explanation.
Question 4:
Illustrate out the term adapted nozzle. Illustrate out the operating principal of such nozzle. Sketch any one type of the adapted nozzle.
Question 5:
Write down the significant factors which must be considered in design and selection of gas turbine combustion chamber?
Question 6:
Illustrate the phenomenon ‘Flame Blow’ in gas turbine combustion chamber. Write down the factors which promote the below out? What are the remedial measures?