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