Numerical model for investigation of the strain distribution in thick composite plates subjected to bolt loads

Author:

Gorjipoor Alireza,Van Hoa Suong,Ganesan Rajamohan

Funder

Natural Sciences and Engineering Research Council of Canada

Ministère du Développement économique de l'Innovation et de l'Exportation (MDEIE)

Le Consortium de recherche et d'innovation en aérospatiale au Québec (CRIAQ)

Bell Helicopter Textron Inc.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Mechanics of Laminated Composite Plates and Shells;Reddy,1997

2. Theories and finite elements for multilayered, anisotropic, composite plates and shells;Carrera;Arch. Comput. Methods Eng.,2002

3. Principles of the Manufacturing of Composite Materials;Van Hoa,2009

4. Design and Analysis of Structural Joints with Composites Materials;Heslehurst,2013

5. Three-dimensional finite element analysis of interlaminar stresses in thick composite laminates;Kim;Comput. Struct.,1991

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