Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction View on Open Library

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

by David S. Dolling

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First published: 1995 1 language
Subjects
Turbulent boundary layer Unsteady flow Boundary layer separation Aerodynamic loads Corner flow Vortex generators Hypersonic boundary layer Boundary layer control Shock wave interaction

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