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, T.J. Coakley.
Contributors: Coakley, T. J.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-201979.; NASA contractor report -- NASA CR-201979.
Publisher: American Institute of Aeronautics and Astronautics; [National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer flow.; Turbulent boundary layer.; Navier-Stokes equation.; Turbulence models.; Shock waves.; Hypersonic speed.; Velocity distribution.; Boundary conditions.; Three dimensional flow.; Three dimensional boundary layer.; Heat transfer.
Other titles: Three dimensional Navier Stokes simulations with two equation turbulence models of intersecting shock waves turbulent boundary layer at Mach 8.3.
Notes: Shipping list no.: 98-0859-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.