A Numerical Integration Based Approach to the Analysis of Shear Deformable Anisotropic Shells of Revolution Subjected to Non-Axisymmetric Loading
Author:
Affiliation:
1. Defence Industries Research and Development Institute
2. Middle East Technical University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2346
Reference26 articles.
1. Stress and vibration analyses of anisotropic shells of revolution
2. A finite element semi-analytical model for laminated axisymmetric shells: statics, dynamics and buckling
3. A semi-analytical finite element model for the analysis of laminated 3D axisymmetric shells: Bending, free vibration and buckling
4. Analysis of Shells of Revolution Subjected to Symmetrical and Nonsymmetrical Loads
5. Numerical analysis of anisotropic rotational shells subjected to nonsymmetric loads
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