Numerical and Experimental Aeroelastic Analysis of High Aspect Ratio Wings .

高展弦比机翼的数值和实验气动弹性分析。

• 批准号: 2611371
• 金额: --
• 依托单位: Brunel University London
• 依托单位国家: 英国
• 项目类别: Studentship
• 财政年份: 2021
• 资助国家: 英国
• 起止时间: 2021 至 无数据
• 项目状态: 未结题
• 来源: https://gtr.ukri.org/projects?ref=studentship-2611371
• 关键词: Numerical; Experimental; Aeroelastic; Analysis; Aspect

This exciting research project is focused on the accurate nonlinear numerical and experimental aeroelastic analysis of flexible wings and explore the use of reduced-order models to ensure the practicability in the use of developed methods for domains with large degrees of freedom. It will also explore the use of high-fidelity numerical modelling, including turbulence modelling. This research is applicable to the aeroelasticity of flexible and large wind turbine blades. The unified scaling law in solid continuum recently developed by the research team here at Brunel will be further developed for experimental investigations during this research project.

这个令人兴奋的研究项目集中在柔性机翼的准确非线性数值和实验性航空弹性分析上，并探索使用降级模型的使用，以确保在使用较大自由度的领域的开发方法中使用可实用性。它还将探索使用高保真数值建模（包括湍流建模）的使用。这项研究适用于柔性和大型风力涡轮机叶片的航空弹性。在此研究项目期间，将进一步开发由Brunel的研究团队开发的实体连续体的统一扩展定律。