Prediction of Free Edge Stresses in Laminate Systems Using Multi-Dimensional Method Based on Higher-Order Modeling

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This paper presents efficient modeling technique using multi-dimensional method for prediction of free edge stresses in laminate plates. For the efficient modeling, the p-convergent transition element based on two-dimensional layer elements is proposed in order to connect discrete layer elements. The elements considered are on the basis of subparametric element concept. The results obtained by this proposed model are compared with those available in literatures. Especially, three-dimensional out-of-plane stresses in the interior and near the free edges are evaluated. The present models using the p-convergent transition element are demonstrated to be more practical and economical than previously p-version FEM using only single element type.

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1260-1263

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September 2011

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] Y.W. Kwon, J.E. Akin, Analysis of layered composite plates using a higher-order deformation theory, Comput. Struct. 27 (1987) 619-623.

DOI: 10.1016/0045-7949(87)90077-0

Google Scholar

[2] P.F. Pai, A.N. Palazotto, A higher-order sandwich plate theory accounting for 3-D stresses, Int. J. Solids Struct. 38 (2001) 5045-5062.

DOI: 10.1016/s0020-7683(00)00356-5

Google Scholar

[3] J.N. Reddy, M. Savoia, Layer-wise shell theory for postbuckling of laminated circular cylindrical shells. AIAA J. 30 (1992) 2148-2154.

DOI: 10.2514/3.11193

Google Scholar

[4] C.R. Dohrmann, S.W. Key, M.W. Heinstein, A method for connecting dissimilar finite element meshes in two-dimensions. Int. J. Numer. Methods Eng. 48, 5 (2000) 655-78.

DOI: 10.1002/(sici)1097-0207(20000620)48:5<655::aid-nme893>3.0.co;2-d

Google Scholar

[5] E. Garusi, A. Tralli, A hybrid stress-assumed transition element for solid-to beam and plate-to-beam connections, Comput. Struct. 80 (2002) 105-115.

DOI: 10.1016/s0045-7949(01)00172-9

Google Scholar

[6] N.U. Ahmed, P.K. Basu, Higher-order finite element modeling of laminated composite plates, Int. J. Numer. Methods Eng. 37 (1994) 123-139.

DOI: 10.1002/nme.1620370109

Google Scholar

[7] J.S. Ahn, P.K. Basu, K.S. Woo, Analysis of cracked aluminum plates with one-sided patch repair using p-convergent layered model, Finite Elem. Anal. Des. 46, 5 (2010) 438-448.

DOI: 10.1016/j.finel.2010.01.008

Google Scholar

[8] K.S. Woo, J.H. Jo, P.K. Basu, J.S. Ahn, Stress intensity factor by p-adaptive refinement based on ordinary Kriging interpolation, Finite Elem. Anal. Des. 45 (2009) 227-234.

DOI: 10.1016/j.finel.2008.10.002

Google Scholar

[9] J.N. Reddy, Mechanics of Laminated Composites Plates and Shells; Theory and Analysis, second ed., CRC Press, New York, (2004)

Google Scholar