Engineering, 17.03.2020 05:21 Jasten
The inlet for a high-bypass-ratio turbofan engine has an area A1 of 6.0 m 2 and is designed to have an inlet Mach number M~ of 0.6. Determine the additive drag at the flight conditions of sea-level static test and Mach number of 0.8 at 12-km altitude.
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The inlet for a high-bypass-ratio turbofan engine has an area A1 of 6.0 m 2 and is designed to have...
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