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Title Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows [electronic resource] / A.R. Porro ... [et al.].

Imprint

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.

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Connect to http://purl.access.gpo.gov/GPO/LPS67809

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:3142	---	Available

Description	26 p. : ill. ; 28 cm.
Series	NASA technical paper ; 3142
Note	"August 1991"--Cover.
Form	Mode of access: Internet via the NTRs web site.
Bibliography	Includes bibliographical references (p. 26).
Subject	Aerodynamics, Hypersonic.
	Aerodynamics, Supersonic.
	Boundary layer.
	Boundary layers.
	Compressible flow.
	Honeycomb structures.
	Hypersonic flow.
	Supersonic flow.
	Turbulent boundary layer.
	Wind tunnel models.
Added Author	Porro, A. R. (A. Robert)
	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:3142