Aero Performance Problem, Other Engineering

Given data for an F-4 (W=40000 lb, S=530 ft^2, Ta@sea level=35800 lb, Mach=1.5, h=20000 ft (std day), Cd0=.0224, k=.1516) find aircraft''s specific excess power in straight-and-level flight
Posted Date: 11/27/2012 12:40:44 PM | Location : United States







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