problem 1:
Critically discuss any two differentiations between turboprop and turbofan engines form operational point of view.
problem 2:
How does thrust developed by a turboject engine vary with the air speed?
problem 3:
What factors prevent stall in inlet diffuser?
problem 4:
How do you diminish the total pressure loss in the design of supersonic inlet?
problem 5:
prepare down the functions of the secondary air in gas turbine combustion chamber