Flow separation in shock wave boundary layer interactions at hypersonic speeds /

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Bibliographic Details
Author / Creator:Hamed, A. (Awatef)
Imprint:Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [1990]
Description:1 volume.
Series:NASA contractor report ; 4274
NASA contractor report ; NASA CR-4274.
Subject:Boundary layer separation.
Boundary layers.
Cylindrical bodies.
Flat plates.
Hypersonic speed.
Oblique shock waves.
Shock wave interaction.
Turbulent boundary layer.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6556199
Hidden Bibliographic Details
Other authors / contributors:Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
Notes:Prepared at the Joint Institute for Advancement of Flight Sciences for Langley Research Center under Contract NAS1-18458.
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.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online)
Govt.docs classification:NAS 1.26:4274