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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

Mechanical Engineering, Engineering

  • Category:- Mechanical Engineering
  • Reference No.:- M912463

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