Proceedings of the ... Congress of the International Council of the Aeronautical Sciences, Volume 20, Issues 1-2
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aerodynamic aeroelastic aerofoil AIAA aircraft airfoil airplane airport algorithm analysis angle of attack application approach blade boundary layer calculated characteristics coefficient combustion combustor components computed configuration developed downburst drag dynamic effect element engine equations Euler evaluation experimental expert system factor fatigue flap flight test flow Fluid flutter frequency fuel function geometry go-around gradient grid high-lift ICAO increase inlet integration interaction investigated inviscid lift lift coefficient linear loads Mach number mass matrix maximum measurements mesh method microburst mode NASA Navier-Stokes Navier-Stokes equations nozzle obtained operating optimization panel parameters performance piezoelectric pilot predicted present pressure distribution procedure propeller ramjet range ratio reduced region Reynolds number rotor sensor shown in Figure simulation solution speed stability stress structure subsonic supersonic surface temperature transonic turbulence model unsteady values variable vector velocity vertical viscous vortex wind tunnel windshear wing