Computation of stress resultants from the element stiffness matrices.
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3614
Reference4 articles.
1. Fig. 1
2. Application of matrix displacement method to linear elastic analysisof shells of revolution.
3. Consistent matrix formulations for structural analysis using finite-element techniques.
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