Question 1:
Mention any four significant operating variables of the gas turbine combustion chamber.
Question 2:
How efficiency of the jet engine nozzle defined?
Question 3:
Critically discuss the concept ‘Optimum Expansion’ in jet engine nozzle operation.
Question 4:
Why is it that the number of phases in compressor is more than that in a turbine of jet engine?
Question 5:
Illustrate out the concept ‘blade loading coefficient’ of compressor.