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Finite element analysis of laminated plates and shells, volume 1The finite element method is used to investigate the static behavior of laminated composite flat plates and cylindrical shells. The analysis incorporates the effects of transverse shear deformation in each layer through the assumption that the normals to the undeformed layer midsurface remain straight but need not be normal to the mid-surface after deformation. A digital computer program was developed to perform the required computations. The program includes a very efficient equation solution code which permits the analysis of large size problems. The method is applied to the problem of stretching and bending of a perforated curved plate.
Document ID
19780016634
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Seide, P.
(University of Southern California Los Angeles, CA, United States)
Chang, P. N. H.
(University of Southern California Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1978
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-157106
Report Number: NASA-CR-157106
Accession Number
78N24577
Funding Number(s)
CONTRACT_GRANT: NSG-1401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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