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Juncture stress fields in multicellular shell structures. Volume V - Influence coefficients of segmental shellsDigital programs to determine stiffness influence coefficients of cylindrical, conical, and spherical shell segments by finite difference method
Document ID
19660007432
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chen, C. T. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Stern, P. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
August 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-70016
M-77-65-6
Report Number: NASA-CR-70016
Report Number: M-77-65-6
Accession Number
66N16721
Funding Number(s)
CONTRACT_GRANT: NAS8-11480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FINITE DIFFERENCE METHOD
CONICAL SHELL
STRESS COMPUTER PROGRAM
SPHERICAL SHELL
CYLINDRICAL SHELL

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