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aerodynamic aerodynamic center aileron aircraft airfoil airload airplane design angle of attack approximately aspect ratio bicycle gear calculated center of gravity characteristics chord coefficient of lift condition critical dCm/dCl decrease deflection determined direct operating cost distance drag coefficient efficient elevator equal Equation equilibrium feet field length flap flight fuel weight fuselage gravity location ground effects high speed high wing horizontal tail increase induced drag jet transport landing field landing gear lift coefficient lift curve low wing Mach number maximum Cl method nacelle number of passengers obtained optimum altitude outrigger parasite drag payload plane presented propeller range rate of climb rear spar shear shown in Figure span spanwise specifications stability and control stick free stringers structural sweepback and thickness tail surfaces take-off weight taper ratio thickness ratio thrust loading tion tires usually variation velocity vertical tail wing area wing loading wing weight zero