Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
By: D.R. Reddy and T.J. Benson and L.J. Weir ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Society of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 1990.
Contributors: Benson, T. J.; Weir, L. J.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 102518.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Number of pages: 13
Subjects: Viscous flow.; Computational fluid dynamics.; Computer programs.; Navier-Stokes equation.; Proving.; Supersonic inlets.; Supersonic wind tunnels.; Turbulence models.; Viscous flow.
Notes: Cover title.

Shipping list no.: 1990-0858-M.

Distributed to depository libraries in microfiche.

"AIAA-90-0600.

Includes bibliographical references (p. 5).

Also available via Internet from the NTRS web site. Address as of 5/1/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900010774%5F1990010774.pdf; current access is available via PURL.

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