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Flugmechanik
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Zonal Navier-Stokes methodology for flow simulation about a complete aircraft
X-59 Sonic Boom Test Results from the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel
X-59 Sonic Boom Test Results from the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel
X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0
X-31 post-stall envelope expansion and tactical utility testing
Wing pressure distributions from subsonic tests of a high-wing transport model
Wing planform effects at supersonic speeds for an advanced fighter configuration
Winglet effectiveness on low aspect ratio wings at supersonic Mach numbers
Winglet and long duct nacelle aerodynamic development for DC-10 derivatives
Wing laminar boundary layer in the presence of a propeller slipstream
Wing flutter calculations with the CAP-TSD unsteady transonic small disturbance program
Wing Download Results from a Test of a 0.658-Scale V-22 Rotor and Wing
Wing-body Combinations with Wings of Very Low Aspect Ratio at Supersonic Speeds