Nonlinear Models for Biologically-Inspired Elastic Membrane Wings
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Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. An arbitrary lagrangian-eulerian finite element method for transient dynamic fluid-structure interactions
2. 3L. Ferguson, E. Aulisa, P. Seshaiyer and R. Gordnier. Computational modeling of highly flexible membrane wings in micro air vehicles. AIAA Paper No. 2006-1661, AIAA/ASME/ASCE/AHS/ASC 47th Structures, Structural Dynamics and Materials Conference, Newport, Rhode Island, May1-4,2006.
3. Micro-Air-Vehicles: Can They be Controlled Better?
4. NUMERICAL ANALYSIS OF SOME DECOUPLING TECHNIQUES FOR THE APPROXIMATION OF THE UNSTEADY FLUID STRUCTURE INTERACTION
5. Lagrangian-Eulerian finite element formulation for incompressible viscous flows
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