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.

这一激动人心的研究项目致力于对柔性机翼进行精确的非线性数值和实验气动弹性分析，并探索使用降阶模型来确保所开发的方法在大自由度区域中的实用性。它还将探索高保真数值模拟的使用，包括湍流建模。该研究适用于柔性和大型风力机叶片的气动弹性。布鲁内尔大学的研究小组最近在固体连续介质中发展的统一标度定律将在本研究项目期间进一步发展用于实验研究。