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Loads induced by terminal-shock boundary-layer interaction on cone-cylinder bodiesLoads induced by terminal shock boundary layer interaction on cone-cylinder bodies, discussing angle of attack effect
Document ID
19700065747
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ericsson, L. E.
Date Acquired
August 5, 2013
Publication Date
September 1, 1970
Subject Category
Aerodynamics
Accession Number
70A41863
Funding Number(s)
CONTRACT_GRANT: NAS8-20354
Distribution Limits
Public
Copyright
Other

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