Comparative analysis and exprimental results of advanced control strategies for vibration suppression in aircraft wings
نویسندگان
چکیده
منابع مشابه
Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams –Dynamics, Stability and Control
Within the basic framework of an existing anisotropic thin-walled beam model, a cou-ple of non-classical effects are further incorporated and the model thereby developed isvalidated. Three types of lay-up configurations, namely, the cross-ply, circumferentiallyuniform stiffness (CUS), and circumferentially asymmetric stiffness (CAS) are investi-gated. The solution methodology is...
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ژورنال
عنوان ژورنال: Journal of Physics: Conference Series
سال: 2017
ISSN: 1742-6588,1742-6596
DOI: 10.1088/1742-6596/783/1/012054