Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

An edition of Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction (1995)

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95

By David S. Dolling

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Publish Date

1995

Publisher

Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin,National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Turbulent boundary layer, Unsteady flow, Boundary layer separation, Aerodynamic loads, Corner flow, Vortex generators, Hypersonic boundary layer, Boundary layer control, Shock wave interaction