A collection of technical papers: AIAA Aircraft Systems Meeting, August 4-6, 1980, Anaheim, California
American Institute of Aeronautics and Astronautics, 1980 - Technology & Engineering
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acquisition aerodynamic AIAA AIAA AIRCRAFT SYSTEMS Air Force aircraft design airfoil airframe airplane analysis angle of attack approach aspect ratio aviation baseline basic capability carrier Cessna characteristics chord components concept configuration cost cruise CTOL cycle deck deflection delta wing drag drag coefficient effect efficiency engine evaluation factor fighter fighter aircraft flap flow fuel function improved increase inlet landing launch leading edge leading-edge droop lift coefficient load logistics Mach number maximum mission nacelle NASA noise nozzle operating outboard Pane parameters percent performance production propeller range reduced Research scale ship shown in Figure simulation spanwise speed spin stall STOL STOVL structural subsonic supersonic surface swept wing takeoff thrust thrust vector tion turbofan turboprop turbulence upwash V/STOL V/STOL aircraft vector velocity vertical vortex VTOL wave drag wind tunnel wing winglets