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Assessment of computational models for multilayered composite shellsA review is made of the different approaches used for modeling multilayered composite shells. Discussion focuses on different approaches for developing two-dimensional shear deformation theories; classification of two-dimensional theories based on introducing plausible displacement, strain and/or stress assumptions in the thickness direction; first-order shear deformation theories based on linear displacement assumptions in the thickness coordinate; and efficient computational strategies for anisotropic composite shells. Extensive numerical results are presented showing the effects of variation in the lamination and geometric parameters of simply supported composite cylinders on the accuracy of the static and vibrational responses predicted by eight different modeling approaches (based on two-dimensional shear deformation theories).
Document ID
19910027177
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Noor, Ahmed K.
(NASA Langley Research Center Hampton, VA, United States)
Burton, W. Scott
(NASA Langley Research Center; George Washington University Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1990
Publication Information
Publication: Applied Mechanics Reviews
Volume: 43
ISSN: 0003-6900
Subject Category
Structural Mechanics
Report/Patent Number
ISSN: 0003-6900
Accession Number
91A11800
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-87-0115
CONTRACT_GRANT: NAG1-788
Distribution Limits
Public
Copyright
Other

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