A 4-node co-rotational ANS shell element for laminated composite structures

Author:

Kim Ki-Du,Lee Chang-Soo,Han Sung-Cheon

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference37 articles.

1. Analysis of thick and thin shell structures by curved finite elements;Ahmad;Int J Numer Meth Eng,1970

2. A stabilized 9-node non-linear shell element;Kebari;Int J Numer Meth Eng,1992

3. Derivation of element stiffness matrices by assumed strain distributions;MacNeal;Nucl Eng Des,1982

4. A continuum mechanics based four-node shell element for general non-linear analysis;Dvorkin;Eng Comput,1984

5. An 8-node assumed strain element with explicit integration for isotropic and laminated composite shells;Kim;Struct Eng Mech,2002

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1. Effect of Stiffness on Flutter of Composite Wings with High Aspect Ratio;Mathematical Problems in Engineering;2021-05-18

2. Modeling Deficiencies in the Eight-Node Mindlin Plate Finite Element Physically Explained;Journal of Engineering Mechanics;2020-02

3. Nonlinear aeroelastic characteristics analysis of composite wing with high aspect ratio based on co-rotational method;Journal of Fluids and Structures;2018-10

4. A 4-node thin shell element based on co-rotational for laminated composite structures;Revista Internacional de Métodos Numéricos para Cálculo y Diseño en Ingeniería;2018-01-01

5. On a Four-Node Quadrilateral Plate for Laminated Composites;Latin American Journal of Solids and Structures;2017-12

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