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