Consistent Third-Order Shell Theory with Application to Composite Cylindrical Cylinders
Author:
Affiliation:
1. Texas A&M University, College Station, Texas, 77843-3123
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.6593
Reference48 articles.
1. Analysis of thick and thin shell structures by curved finite elements
2. On a stress resultant geometrically exact shell model. Part I: Formulation and optimal parametrization
3. Hierarchic finite elements for thin Naghdi shell model
4. Development of geometrically exact new shell elements based on general curvilinear co-ordinates
5. MITC elements for a classical shell model
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