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Juncture Stress Fields in Multicellular Shell Structures. Volume VI - Analysis of Multicellular Propellant Pressure Vessels by the Stiffness Method Final ReportMatrix algebra solution, using coordinate systems transformations, to boundary value problem for structures composed of shell elements
Document ID
19660007688
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
November 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-70187
M-77-65-7
Report Number: NASA-CR-70187
Report Number: M-77-65-7
Accession Number
66N16977
Funding Number(s)
CONTRACT_GRANT: NAS8-11480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHELL
COORDINATE TRANSFORMATION
BOUNDARY VALUE PROBLEM
MATRIX ALGEBRA
STRUCTURAL DYNAMICS

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