ICAS proceedings: ... Congress of the International Council of the Aeronautical Sciences. 9 - 14 September 1990, Stockholm, Sweden, Volume 11; Volume 17
American Inst. of Aeronautics and Astronautics, 1990 - Aeronautics - 1193 pages
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ICAS9 00 4 The X31 and Advanced Highly Manoevrable Aircraft
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2-D testing acoustic adaptive wall aerodynamic aeroelastic Aeronautical AIAA aircraft airfoil analysis angle of attack AWTS beam blade forces boundary layer calculated chord coefficient composite configuration constraints cruise divergence boundary downstream effects eigenvalues engine equation evacuations experimental Figure flexible walls flight tests flow field flutter free stream frequency function fuselage increase influence interaction iterative laminar flow lift lift coefficient linear loading Mach number maximum measurements method microphone nacelle NASA noise nozzle optimization parameters performance perturbations pilot pitch plane prediction pressure distribution probe problem propeller Propfan proprotor ratio reduced Reynolds number rotating rotor sensors shear shown in Fig simulation slipstream solution sound power levels speed stability static pressure structural supersonic surface techniques test section thrust tion transition transonic turbulence unsteady values vector velocity vortex vortex system vortices wake wave wind tunnel wing