Numerical and Experimental Aeroelastic Analysis of High Aspect Ratio Wings .

这个令人兴奋的研究项目的重点是精确的非线性数值和实验气动弹性分析的柔性机翼和探索使用降阶模型，以确保在使用开发的方法与大自由度域的实用性。它还将探讨使用高保真数字模型，包括湍流模型。该研究适用于柔性大型涡轮机叶片的气动弹性分析。在固体连续统一的标度律最近开发的研究小组在布鲁内尔大学将进一步发展的实验研究在这个研究项目。

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.