3D visualization of unsteady 2D airplane wake vortices

By Kwan-Liu Ma

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Publish Date

1994

Publisher

Institute for Computer Applications in Science and Engineering, NASA Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Wing tip vortices, Numerical flow visualization, Aircraft wakes, Ground effect (Aerodynamics), Rolling moments, Hilsch tubes