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Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /

Bibliographic Details
Main Authors:	Stallings, Robert L. (Author), Lamb, Milton (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:	NASA technical paper ; 1789.
Subjects:	Boundary layer flow. Boundary layer stability. Heat transfer. Reynolds number. Wind tunnel tests. Aerothermodynamics. Boundary layer. Supersonic wind tunnels.
Online Access:	https://purl.fdlp.gov/GPO/gpo71443

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