A Collection of Technical Papers: AIAA 4th Aircraft Design, Flight Test, and Operations Meeting, Los Angeles, California, August 7-9, 1972
American Institute of Aeronautics and Astronautics, 1972 - Aeronautics
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aerodynamic AIAA aileron airborne Aircraft Design airfoil airline airplane airport altitude analysis angle of attack approach speed area navigation basic beam Blown Flap bypass ratio capability Center characteristics coefficient configuration control system cost cruise curve deflection derivatives determined drag Dutch roll dynamic effects engine evaluation factor flap flight test flow flutter force frequency function fuselage glide slope gust improved increase input landing gear lift lift coefficient loads Mach number maneuver maximum methods mission mode modules nacelle NASA noise level normal nozzle obtained operating panel parachute parameters payload percent performance phugoid pilot pitch pressure problem proprotor range ratio reduced roll rotor runway shown in Figure simulation spanwise blowing spin spoilers stability static STOL STOL aircraft STOLport structural surface tail takeoff techniques thrust reversers tion transport V/STOL velocity vertical wind tunnel wing