Engineering Analysis of Flight Vehicles |
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aerodynamic aileron aircraft airfoil altitude angle of attack applied approach approximation assume atmosphere body boundary calculated Chapter coefficient components constant corresponding defined derivatives determined direction discussed drag dynamic effects efficiency elevator engine entry equations estimate example Figure fixed flight flow force formula function given important initial instance integral lateral leading lift limit linear loading Mach mass maximum mode moment motion needed normal Note observe obtain operation parameters performance pitching plane positive pressure problem proportional quantities range ratio reference relation relative respect rolling rotation shape shows solution speed stability subsonic supersonic surface theory thrust trim turn typical unit variable vector vehicle vertical weight wing zero