Nonlinear Aeroelastic Framework Based on Vortex-Lattice Method and Corotational Shell Finite Element
Authors:
- Carlos de SouzaCSCarlos de Souza
- Roberto Gil da SilvaRSRoberto Gil da Silva
- Carlos CesnikCCCarlos Cesnik
- 23 April 2012
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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