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Conical shell deflection and acceleration response program /darc/IBM 7094 computer program for calculation of truncated conical shell deflection and acceleration response
Document ID
19650024773
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brunkow, A. T.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
August 2, 2013
Publication Date
July 30, 1965
Subject Category
Structural Mechanics
Report/Patent Number
B731
NASA-CR-66013
Report Number: B731
Report Number: NASA-CR-66013
Accession Number
65N34374
Funding Number(s)
CONTRACT_GRANT: NAS1-3179
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DEFLECTION
CONICAL SHELL
ACCELERATION
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