Study of interlaminar stresses in composite laminates subjected to torsional loading
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作者:
Mitchell, J.A.
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机构:
Sandia National Laboratory, MS 0443, P.O. Box 5800, Albuquerque, NM 87185-0443, United StatesSandia National Laboratory, MS 0443, P.O. Box 5800, Albuquerque, NM 87185-0443, United States
Mitchell, J.A.
[1
]
Reddy, J.N.
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h-index: 0
机构:
Sandia National Laboratory, MS 0443, P.O. Box 5800, Albuquerque, NM 87185-0443, United StatesSandia National Laboratory, MS 0443, P.O. Box 5800, Albuquerque, NM 87185-0443, United States
Reddy, J.N.
[1
]
机构:
[1] Sandia National Laboratory, MS 0443, P.O. Box 5800, Albuquerque, NM 87185-0443, United States
来源:
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1600年
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American Inst. Aeronautics and Astronautics Inc.卷
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39期
A computational procedure for accurate determination of interlaminar stresses in thick and thin composite laminates subjected to torsional loading is presented. A multilevel, recursively defined preconditioner in conjunction with the preconditioned conjugate gradient (PCG) algorithm is constructed from a sequence of hierarchical vector spaces arising from the p-version of the finite element method. The computational procedure is used to model stress fields in thick and thin laminates in torsion using three-dimensional and quasi-three-dimensional models. Results indicate that the preconditioner developed here can be used to produce an efficient iterative solver for the determination of two- and three-dimensional stress fields in composite structures.