Module 15 Gas Turbine Engine Practice Questions - UK CAA Part-66 AME Module 15 - Gas Turbine Engine Exam

How is Gross Thrust ($F_g$) defined for a gas turbine engine operating under static conditions?

Total thrust produced by exhaust gas momentum plus nozzle pressure differential force, without subtracting inlet ram drag Net thrust remaining after airframe parasite drag subtraction Thrust produced exclusively by the fan rotor in a high-bypass turbofan Difference between total exhaust momentum and incoming ram momentum

Correct Answer:

Total thrust produced by exhaust gas momentum plus nozzle pressure differential force, without subtracting inlet ram drag

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