A collection of technical papers: AIAA 6th Aircraft Design, Flight Test and Operations Meeting, Los Angeles, California, August 12-14, 1974
American Institute of Aeronautics and Astronautics. - Technology & Engineering
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acoustic aerodynamic Aeronautics and Astronautics AIAA airfoil airframe airline airplane airport altitude analysis angle of attack baseline Boeing boundary layer braking bypass ratio capability characteristics configuration core engine noise cost cruise deflection distance drag duct dynamic effect ejector energy intensity evaluation feet Flight Dynamics Flight Test flow force frequency friction fuel fuselage glide slope glideslope hydroplaning increase incremental inlet IPAD jet flap landing lift coefficient Mach number maneuver maximum method Mu-Meter nacelle NASA nozzle operational performance pilot prediction pressure distribution problem procedure propulsion ratio reduced reverse thrust runway runway surface scramjet shear shown in Figure simulation speed static STOL stress structure suppressor takeoff temperature thrust tion tire touchdown trailing edge transport turbine two-segment approach upper segment V/STOL values vehicle vertical vortex weight wheel wind wind shear wing