Mach 6 flow field surveys beneath the forebody of an airbreathing missile /

Bibliographic Details
Main Authors:	Johnston, Patrick J. (Author), Hunt, James L. (James Larry), 1939- (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, March 1986.
Series:	NASA technical paper ; 2491.
Subjects:	Boundary layers. Flow distribution. Reynolds number. Wind tunnel tests. Mach number. Guided missiles > Aerodynamics. Aerodynamics, Hypersonic. Boundary layer.
Online Access:	https://purl.fdlp.gov/GPO/gpo105939

Available Online