Effect of ply angle on nonlinear static aeroelasticity of high-aspect-ratio composite wing
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15 صفحه اولStatic and Dynamic Aeroelastic Analysis of a High Aspect Ratio Wing through CFD-CSD Coupled Method
The Solar powered unmanned aircraft have a high-aspect-ratio wings because SPUAV must satisfy the requirement of long endurance and high lift-drag ratio. Therefore, the structure of SPUAV‘s wings are structurally very flexible. The very high flexible wing might have large deformation and many aeroelastic problems. In this paper have a static/dynamic aeroelastic analysis through CFD-CSD coupled ...
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ژورنال
عنوان ژورنال: Journal of Vibroengineering
سال: 2020
ISSN: 1392-8716,2538-8460
DOI: 10.21595/jve.2019.20968