Flow separation in shock wave boundary layer interactions at hypersonic speeds
By: A. Hamed.
Contributors: Joint Institute for Advancement of Flight Sciences.; Langley Research Center.
Series: NASA contractor report -- 4274.; NASA contractor report -- NASA CR-4274.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service
Published: 1990
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer separation.; Boundary layers.; Cylindrical bodies.; Flat plates.; Hypersonic speed.; Oblique shock waves.; Shock wave interaction.; Turbulent boundary layer.
Notes: Prepared at the Joint Institute for Advancement of Flight Sciences for Langley Research Center under Contract NAS1-18458.

Also available via Internet from the NASA Technical Report Server web site. Address as of 7/12/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900006569%5F1990006569.pdf:; current access is available via PURL.

Microfiche. [Wahington, D.C. National Aeronautics and Space Administration, 1990]. 1 microfiche.