Supplementary data for the publication: Experimental Aeroelastic Characterization of a Very Flexible Wing in Steady and Unsteady Inflow

This data set contains experimentally determined aerodynamic loads and structural deflection measurements of the wind tunnel tests of the Delft-Pazy wing conducted in November 2020. The data is intended to be used for validating numerical aeroelastic models. An example FEM model is provided. More information can be found in the linked publication: Experimental Aeroelastic Characterization of a Very Flexible Wing in Steady and Unsteady Inflow (SciTech 2022 conference)<br>

本数据集包含2020年11月开展的代尔夫特-帕齐（Delft-Pazy）机翼风洞试验的实测气动载荷与结构挠度测量数据。本数据集旨在用于验证数值气动弹性模型，并附带了有限元模型（Finite Element Method, FEM）示例。更多详细信息可参阅关联发表论文：《定常与非定常来流下超柔性机翼的气动弹性特性实验表征》（SciTech 2022会议）