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Author

Hamed, A. (Awatef)

Title Flow separation in shock wave boundary layer interactions at hypersonic speeds [electronic resource] / A. Hamed.

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].

Connect to
Connect to https://permanent.fdlp.gov/lps61576/lps61576/ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900006569_1990006569.pdf

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.26:4274	---	Available

Description	1 v.
Series	NASA contractor report ; 4274
	NASA contractor report ; NASA CR-4274.
Note	Prepared at the Joint Institute for Advancement of Flight Sciences for Langley Research Center under Contract NAS1-18458.
Form	Mode of access via the NTRS web site.
Subject	Boundary layer separation.
	Boundary layers.
	Cylindrical bodies.
	Flat plates.
	Hypersonic speed.
	Oblique shock waves.
	Shock wave interaction.
	Turbulent boundary layer.
Added Author	Joint Institute for Advancement of Flight Sciences.
	Langley Research Center.
Gpo Item No.	0830-H-14 (online)
Sudoc No.	NAS 1.26:4274