A Collection of Technical Papers: AIAA 5th Aircraft Design, Flight Test and Operations Meeting, St. Louis, Missouri, August 6-8, 1973American Institute of Aeronautics and Astronautics, 1973 - Aeronautics |
Contents
GENERAL PURPOSE DIGITAL COMPUTER | |
GO AHEAD | |
TACTICAL COORDINATOR | |
Copyright | |
6 other sections not shown
Common terms and phrases
acoustic aerodynamic aerospace AIAA aileron Aircraft Design aircraft noise airfoil airplane airport altitude analysis angle of attack approach baseline blown flap Boeing boundary layer bypass capability coefficient component concept configuration control system cost crosswind landing cruise deflection drag DSFC duct Dutch roll dynamic effect ejector engine EPNdB evaluation fighter flight test flow frequency fuel fuselage gross weight hydrogen hypersonic improvements increased inlet jet noise JT8D lift coefficient load located Mach number maneuver maximum minimum nacelle NASA noise levels noise reduction nozzle operating parameters payload performance pilot rating pitch polyimide pressure distribution problem propulsion range reduced Refan retrofit Reynolds number rudder shown in Figure side force control sideline sideslip simulated sonic boom speed stability stall strip static STOL structure subsonic supersonic surface takeoff temperature thrust tion transducer transonic transport turbulence vehicle velocity vertical wind tunnel wing