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Physics, 02.12.2020 19:00 aron4327

Determine the coefficient of lift given the following info. A Gulfstream G280 has a wing area of 46m^2. Its total mass during a particular flight is 13,500kg at its current altitude is 0.28 kg Im^3. and is cruising at B40km/hr. The air density

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Determine the coefficient of lift given the following info. A Gulfstream G280 has a wing area of 46m...
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