Gust Load Alleviation including Geometric Nonlinearities Based on Dynamic Linearization of Structural ROM
This paper describes a framework for an active control technique applied to gust load alleviation (GLA) of a flexible wing, including geometric nonlinearities. Nonlinear structure reduced order model (ROM) and nonplanar double-lattice method (DLM) are used for structural and aerodynamic modeling. Th...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Wiley
2019-01-01
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| coleção: | International Journal of Aerospace Engineering |
| Acesso em linha: | http://dx.doi.org/10.1155/2019/3207912 |
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