Study of interlaminar stresses in composite laminates subjected to torsional loading

Citation
Ja. Mitchell et Jn. Reddy, Study of interlaminar stresses in composite laminates subjected to torsional loading, AIAA J, 39(7), 2001, pp. 1374-1382
Citations number
30
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
39
Issue
7
Year of publication
2001
Pages
1374 - 1382
Database
ISI
SICI code
0001-1452(200107)39:7<1374:SOISIC>2.0.ZU;2-J
Abstract
A computational procedure for accurate determination of interlaminar stress es in thick and thin composite laminates subjected to torsional loading is presented. B multilevel, recursively defined preconditioner in conjunction with the preconditioned conjugate gradient (PCG) algorithm is constructed f rom a sequence of hierarchical vector spaces arising from the p-version of the finite element method. The computational procedure is used to model str ess fields in thick and thin laminates in torsion using three-dimensional a nd quasi-three-dimensional models. Results indicate that the preconditioner developed here can be used to produce an efficient iterative solver for th e determination of two- and three-dimensional stress fields in composite st ructures.