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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 radii

Author
Blakemore, T. L.
Published
Jun 28, 1961.
Physical Description
1 electronic document
Additional Creators
Mayo, E. A.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Newtonian aerodynamic coefficients for predicting hypersonic stability characteristics of reentry bodies with various heat shield, afterbody angle and edge geometries
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19700025216.
Accession ID: 70N34532.
NASA-TM-X-64332.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15951128