Flapping-Wing Structural Dynamics Formulation Based on a Corotational Shell Finite Element
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. U. S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Dayton, Ohio 45440
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050494
Reference42 articles.
1. Flexural stiffness in insect wings I. Scaling and the influence of wing venation
2. Support and deformability in insect wings
3. Computational strategies for flexible multibody systems
4. Corotational non-linear analysis of thin plates and shells using a new shell element
5. An efficient facet shell element for corotational nonlinear analysis of thin and moderately thick laminated composite structures
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