An analysis of supersonic flows with low-Reynolds number compressible two-equation turbulence models using LU finite volume implicit numerical techniques
By: J. Lee.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 195302.; NASA contractor report -- NASA CR-195302.
Publisher: National Aeronautics and Space Administration
Published: 1994
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: K-epsilon turbulence model.; Low Reynolds number.; Shock wave interaction.; Supersonic flow.; Turbulent boundary layer.; Turbulent flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0863-M.

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