Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /

Bibliographic Details
Main Authors:	Nowak, Robert J. (Author), Albertson, Cindy W. (Author), Hunt, L. Roane (Lewis Roane) (Author)
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1985.
Series:	NASA technical paper ; 2345.
Subjects:	Flow distribution. Cones. Aerodynamic heating. Boundary layer transition. Turbulent boundary layer. Angle of attack (Aerodynamics) Noses (Aircraft) Reynolds number. Aerothermodynamics.
Online Access:	https://purl.fdlp.gov/GPO/gpo93362

Description
Item Description:	"January 1985." Prepared at Langley Research Center.
Physical Description:	1 online resource (87 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 19-21).