Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
By: Kamlesh Kapoor, Bernard H. Anderson.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106579.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Computer programs.; Finite volume method.; Flat plates.; Laminar boundary layer.; Navier-Stokes equation.; Shock wave interaction.; Supersonic inlets.; Three dimensional boundary layer.; Three dimensional models.; Turbulent boundary layer.; Wedges.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0059-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.