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Flight dynamics
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dynamics
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X-31 post-stall envelope expansion and tactical utility testing
Winglet and long duct nacelle aerodynamic development for DC-10 derivatives
Wing flutter calculations with the CAP-TSD unsteady transonic small disturbance program
Wing-alone aerodynamic characteristics at high angles of attack
Wing aerodynamic loading caused by jet-induced lift associated with STOL-OTW configurations
Wind-US Results for the AIAA 1st Propulsion Aerodynamics Workshop
Wind tunnel tests of a 20 inch diameter 1.15 pressure ratio fan engine model
Wind tunnel tests of a 20 inch diameter 1.15 pressure ratio fan engine model