Concepedia

Abstract

Abstract A finite element model is proposed to perform stress analysis for thick curved beams and panels subjected to various types of loadings. The model has 18 nodes in a three‐dimensional cylindrical co‐ordinates system. Three stress components on radial surface (σ rr , τ rθ , and τ rz ) and three displacement components ( u r , u θ , and u z ) are used as nodal degrees of freedom. Therefore, the continuity condition for both stresses and displacements is achieved in the radial direction. Formulation of nodal shape functions and equilibrium equations are based on three‐dimensional elasticity theory and a minimum potential energy method. The accuracy of the method is verified with the standard test problems and exact solutions from the theory of elasticity. The model shows no locking phenomena. Convergence is investigated and the application to layered composite panel is illustrated. Copyright © 2003 John Wiley & Sons, Ltd.

References

YearCitations

1985

3.8K

1970

1.1K

1985

1K

1995

499

1987

381

1978

359

1971

326

1982

242

1964

238

1982

237

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