Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model

An edition of Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model (1994)

Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model

By Stacey J. Cotton

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Publish Date

1994

Publisher

National Aeronautics and Space Administration, Dryden Flight Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Aerodynamic characteristics, Angle of attack, Buffeting, Flight tests, Flow visualization, Liquid-vapor interfaces, Scale models, Sideslip, Stabilizers (Fluid dynamics), Tail assemblies, Vortices, Water tunnel tests, X-29 aircraft