Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations

Author:

Demasi Luciano,Livne Eli

Publisher

American Institute of Aeronautics and Astronautics

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Nonlinear Static Aeroelasticity of High-Aspect-Ratio-Wing Aircraft by Finite Element and Multibody Methods;Journal of Aircraft;2017-03

2. Nonlinear Static Aeroelasticity of High Aspect Ratio Wing Aircraft by FEM and Multibody methods;15th Dynamics Specialists Conference;2016-01-01

3. A Hybrid Quasi-steady CFD-Inflow Approach for Gust Response Analysis of Highly Flexible Aircraft;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

4. Dynamic Aeroelasticity Coupling Full Order Geometrically Nonlinear Structures and Full Order Linear Unsteady Aerodynamics - The Joined Wing Case;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

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