Three dimensional solution of pneumatic active control of forebody vortex asymmetry

An edition of Three dimensional solution of pneumatic active control of forebody vortex asymmetry (1995)

Three dimensional solution of pneumatic active control of forebody vortex asymmetry

By Osama A. Kandil

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Publish Date

1995

Publisher

American Institute of Aeronautics and Astronautics,[National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Angle of attack, Finite volume method, Flux difference splitting, Forebodies, Navier-Stokes equation, Pneumatic control, Tangential blowing