Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions

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Author

Kamlesh Kapoor

Contributions

United States. National Aeronautics and Space Administration. - Contributor

Publication

1994 - National Technical Information Service, distributor, Washington, DC, District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

OCLC Control Number32158036
Open LibraryOL17790154M

Subjects

Topics

Wedges Flat plates Computer programs Supersonic inlets Finite volume method Navier-Stokes equation Shock wave interaction

Series Statement

NASA technical memorandum -- 106579.

Other Editions

Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactionsMicroformNational Technical Information Service, distributor1994-01-01

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