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

Bibliographic Details
Main Author:	Hamed, A. (Awatef)
Corporate Authors:	Joint Institute for Advancement of Flight Sciences, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [1990]
Series:	NASA contractor report ; NASA CR-4274.
Subjects:	Boundary layer separation. Boundary layers. Cylindrical bodies. Flat plates. Hypersonic speed. Oblique shock waves. Shock wave interaction. Turbulent boundary layer.
Online Access:	https://purl.fdlp.gov/GPO/LPS61576

Description
Item Description:	Prepared at the Joint Institute for Advancement of Flight Sciences for Langley Research Center under Contract NAS1-18458. Microform.
Physical Description:	1 volume 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.