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Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3

Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3

By J. E. Bardina

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Publish Date

1994

Publisher

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

Language

eng

Pages

-