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Calculation of hypersonic flow over bodies of revolution at small angles of attack.First order yaw effects on hypersonic air flow about bodies of revolution
Document ID
19650037857
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rakich, J. V.
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 64-430
Report Number: AIAA PAPER 64-430
Accession Number
65A20561
Distribution Limits
Public
Copyright
Other
Keywords
HYPERSONIC FLOW
FLOW FIELD
YAW

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