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aerodynamic AIAA AIAA AIRCRAFT SYSTEMS aileron airfoil airframe airplane altitude analysis angle of attack axisymmetric baseline blowing CADAM canard capability centerbody characteristics chord components concept configuration control system cost cruise deflection delta wing drag drag coefficient dutch roll dynamic effects engine fighter flap flight test flow force fuel fuselage geometry ground high lift HiMAT improved increased induced drag inlet integrated leading edge leading-edge lift coefficient load Mach number maximum measured missile NACA nacelle NASA nozzle operation panel parameters payload performance pilot pitching predicted pressure propulsion radar recovery reduced Reynolds number roll shown in Figure spanwise speed spin spoiler stability stall static strake structural subsonic supersonic surface tail takeoff techniques temperature thrust vectoring tion trailing edge transonic trim V/STOL vehicle velocity vertical vortex lift weight wind tunnel wing winglet