AIAA Aircraft Design Systems Meeting: 92-4251

ACSYNT aerodynamic Aeronautics and Astronautics Aerospace AIAA AIAA Aircraft Design Airbus Aircraft Design Systems airfoil airlift analysis angle augmentation ratio B-spline blade Boeing Sikorsky calculated CHIMP Comanche component concept configuration course cross-section cruise curve cycle delta wing developed diameter duct dynamic ejector nozzle ejector system engine equations evaluation exit Figure flight test flow visualization flowfields forecast frequency fuel fuselage grid ground effect ground vortex gyro helicopter helicopter rotor hover ice impact increase infrared inlet Institute of Aeronautics integrated KHOV lift coefficient lift loss load Lockheed main rotor maximum MHATE mission mode NASA Nondimensional Northrop OARF operating parameters percent performance plane power required Propfan propulsion provides rotor/wing simulation speed stability static STOPDEC/RWB STOVL structural SuperCobra surface tail rotor turbine turbofan turbojet V/STOL vector velocity ventral nozzle vertical thrust weight