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Juncture stress fields in multicellular shell structures. Volume VII - Buckling analysis of segmental orthotropic cylinders under uniform stress distribution Final reportTheoretical solution for buckling problem of orthotropic cylindrical panels under axial compression
Document ID
19660007095
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Almroth, B. O. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Pittner, E. V. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Sobel, L. H. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-69870
LMSC-M-77-65-3
Report Number: NASA-CR-69870
Report Number: LMSC-M-77-65-3
Accession Number
66N16384
Funding Number(s)
CONTRACT_GRANT: NAS8-11480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CURVED PANEL
ORTHOTROPIC CYLINDER
COMPRESSION BUCKLING
AXIAL LOAD

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