Q1 For a typical turbofan engine, indicate true [T] or false [F] after each statement about its operation listed below i
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Q1 For a typical turbofan engine, indicate true [T] or false [F] after each statement about its operation listed below i
statement about its operation listed below in square bracket. 1) For the same pressure ratio, the actual turbine produces less work than the reversible adiabatic one. 2) When the propulsive efficiency of an aero-engine reaches 1 on a jet powered aircraft, it produces the maximum thrust for the aircraft. [ ] 3) In a compressor stage, the rotor increases the absolute velocity of the working fluid. [ ] 4) The aviation fuel must be vaporized and then mixed with air for burning. [ ] 5) In a turbo-engine, the energy of the working fluid is extracted by the turbine. [ ] 6) For a given thrust requirement, a low velocity difference requires a large mass flow rate of air. [ ]
Q1 For a typical turbofan engine, indicate true [T] or false [F] after each