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Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71Wind tunnel investigation of pressure distribution on blunted 15 deg half-cone wedge lifting-entry body
Document ID
19680012212
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Couch, L. M. (NASA Langley Research Center Hampton, VA, United States)
Morris, W. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4494
Report Number: NASA-TN-D-4494
Accession Number
68N21681
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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