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Hypersonic viscous effects on free-flight slender cones.Wind tunnel free flight testing technique to obtain data on hypersonic viscous effects on slender cones
Document ID
19650053701
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Dayman, B., Jr.
Date Acquired
August 2, 2013
Publication Date
August 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 64-46
Report Number: AIAA PAPER 64-46
Accession Number
65A36405
Distribution Limits
Public
Copyright
Other
Keywords
SLENDER CONE
VISCOUS DRAG
WIND TUNNEL STABILITY TEST
HYPERSONIC FLOW

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