Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
By: Kamlesh Kapoor, Bernhard H. Anderson, and Robert J. Shaw.
Contributors: Anderson, Bernhard H.; Shaw, Robert J. 1946-; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106580.
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.; Corner flow.; Hypersonic inlets.; Hypersonic speed.; Inlet flow.; Shock wave interaction.; Supersonic speed.; Turbulent boundary layer.; Two dimensional flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0273-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.