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

Bibliographic Details
Main Author: Bardina, J. E
Corporate Author: United States National Aeronautics and Space Administration
Other Authors: Coakley, T. J
Format: Government Document Book
Language:English
Published: Washington, D.C. : Springfield, Va. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1994]
Series:NASA contractor report NASA CR-201979
Subjects:

Internet

Stanford University

Holdings details from Stanford University
Call Number: NAS 1.26:201979