A Collection of Technical Papers: AIAA/NASA Ames VSTOL Conference, December 7-9, 1981, Palo Alto, California
American Institute of Aeronautics and Astronautics, 1981 - Short take-off and landing aircraft
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aerodynamic airfoil airplane altitude Ames Research Center angle of attack approach augmentation augmentor baseline blade canard capability characteristics compressor concept configuration control system core cost cruise CTOL deflection drag duct dynamic effects ejector engine exhaust fighter flight control flow fuel fuselage gross weight ground ground effect helicopter hover impingement inboard increase installed landing lift coefficient loading Mach number maximum method missiles mission mode nacelle NASA nozzle operating percent performance pilot pitch prediction pressure ratio propulsion control propulsion system QSRA radius range reverse thrust Root chord shown in figure simulation spanwise speed stability static STOL STOVL subsonic supersonic surface takeoff temperature thrust modulation thrust reversing thrust vectoring tilt rotor tion transition turbofan V/STOL aircraft vane variable vector angle vectored thrust velocity vertical tail vortex VTOL wind tunnel wing