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Non-linear analysis of tapered (in steps) laminated plate under uniform inplane load

✍ Scribed by C.M.L. Wu


Publisher
Elsevier Science
Year
1987
Tongue
English
Weight
780 KB
Volume
7
Category
Article
ISSN
0263-8223

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A load increment procedure has been presented to integrate with the ΓΏnite strip method for the post-buckling analysis of laminated plates when subjected to uniform end shortening. In-plane loads are introduced to re ect the end shortening e ect. The Newton-Raphson procedure is implemented to attend