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Aerospace Engineering
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Propulsion MCQ
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The bypass ratio in a turbofan engine is define...
The bypass ratio in a turbofan engine is defined as:
A. Air mass bypassing the engine to air mass passing through core
B. Fuel-air ratio
C. Thrust-weight ratio
D. Compressor pressure ratio
Explanation:
Bypass ratio = mass flow of bypass air / mass flow through core.
Tags:
Propulsion MCQ
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Aerospace Engineering
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