Simulation of glancing shock wave and boundary layer interaction
By: Ching-Mao Hung.
Contributors: Ames Research Center.
Series: NASA technical memorandum -- 102233.
Publisher: National Aeronautics and Space Administration, Ames Research Center; For sale by the National Technical Information Service
Published: 1989
Place of publication: Moffett Field, Calif; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 10
Subjects: Shock waves -- Mathematical models.; Laminar boundary layer.; Boundary layer separation.; Computational fluid dynamics.; Computerized simulation.; Fins.; Shock waves.; Three dimensional flow.
Notes: Shipping list no.: 90-0398-M.

"September 1989."

"A-89241"--Technical rept. documentation p.

Includes bibliographical references (p. 6-7).

Also available via Internet from the NASA Technical Report Server web site. Address as of 8/29/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002654%5F1990002654.pdf; current access available via PURL.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

505-60.