Module 15 Practice Questions - EASA Part-66 Module 15 - Gas Turbine Engine Exam

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Gross thrust of a turbojet at a given operating point is calculated, ignoring fuel mass, as the mass flow multiplied by the jet velocity. Net thrust is obtained by:

Adding the ram drag (intake momentum drag) to the gross thrust Multiplying gross thrust by the bypass ratio Subtracting the ram drag (intake momentum drag) from the gross thrust Dividing gross thrust by the engine pressure ratio

Correct Answer:

Subtracting the ram drag (intake momentum drag) from the gross thrust

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