TECHNICAL PAPERS
Apr 1, 2008

Stiffness Matrices of Isoparametric Four-Node Finite Elements by Exact Analytical Integration

Publication: Journal of Aerospace Engineering
Volume 21, Issue 2

Abstract

Explicit algebraic expressions needed to compute element stiffness matrices using procedural (FORTRAN) and object oriented (C++) computer programs are presented. Numerical illustrations for a convex quadrilateral and a triangle with a side node are included. The wide controversy due to conventional element level approximate numerical quadrature within the computational square domain in η and ξ coordinates is completely resolved here by the closed form analytical integration within the physical element, in x and y coordinates.

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Acknowledgments

The research was supported by the following grants from the National Science Foundation: “Concave Finite Element Shape Functions” NSFCMS-0202232. “Workshop for Scientists and Engineers on Structural Deformations at the Historic Site of Angkor, in Cambodia” NSFOISE-0456406, and “US-France Cooperative Research: Engineering Shape Calculation for Surgery, Biology and Anthropology” NSFINT-0233570.

References

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Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 21Issue 2April 2008
Pages: 45 - 50

History

Received: Mar 31, 2005
Accepted: Sep 2, 2006
Published online: Apr 1, 2008
Published in print: Apr 2008

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Authors

Affiliations

Gautam Dasgupta, M.ASCE [email protected]
Professor, Civil Engineering and Engineering Mechanics, Columbia Univ., 620 S. W. Mudd, 500 West 120 St., New York, NY 10027. E-mail: [email protected]

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