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Investigation of Newtonian static longitudinal aerodynamic characteristics of bodies of revolution with various heat-shield curvatures, afterbody angles, and corner-edge radiiNewtonian aerodynamic coefficients for predicting hypersonic stability characteristics of reentry bodies with various heat shield, afterbody angle and edge geometries
Document ID
19700025216
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blakemore, T. L. (NASA Langley Research Center Hampton, VA, United States)
Mayo, E. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 28, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-64332
Report Number: NASA-TM-X-64332
Accession Number
70N34532
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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