Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions [microform] / Kamlesh Kapoor, Bernard H. Anderson.

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Bibliographic Details
Main Author:	Kapoor, Kamlesh
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], [1994]
Series:	NASA technical memorandum ; 106579.
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.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:106579
NAS 1.15:106579	Restricted Place a Hold