Computational modeling and validation for hypersonic inlets
By: Louis A. Povinelli ; prepared for the 75th Symposium on Hypersonic Combined Cycle Propulsion sponsored by the Propulsion and Energetics Panel of AGARD, Madrid, Spain, May 28-June 1, 1990.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103111.
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Hypersonic -- Research -- United States.; Coputational fluid dynamics.; Hypersonic inlets.; Inlet flow.; Navier-Stokes equation.; Shock wave interaction.; Turbulence models.
Notes: Cover title.

Includes bibliographical references (p. 4).

Also available via Internet from the NASA Technical Report Server web site. Address as of 8/4/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012695%5F1990012695.pdf ; current access is available  via PURL.

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