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Two approximate solutions of the hypersonic blunt-body problem.Axisymmetric blunt bodies shock standoff distances in hypersonic flow determined by numerical and analytic methods
Document ID
19670050327
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gudikunst, A. C.
Huckins, E. K., III
Date Acquired
August 3, 2013
Publication Date
February 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aerodynamics
Accession Number
67A29056
Distribution Limits
Public
Copyright
Other
Keywords
FLOW EQUATION
SHOCK WAVE
BLUNT BODY
HYPERSONIC FLOW
STAGNATION POINT

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