Wind tunnel data set with a wing at all angles of attack

This wind tunnel data set was collected at OJF in TU Delft. The aerodynamic forces and moments of a modified MH32 wing at all angles of attack for different flap deflections and 0%, 70% throttle settings are recorded in this data set. This data set should be valuable for the research on tailsitters, especially the impact of inverse flow on the tailsitters in the descending phase. <br> The repeated experiment data for 0% throttle on Feb 24, 2021 are also provided as a supplement to validate the accuracy of the measurements. <br> The dataset is related to the article ''Wind tunnel tests of a wing at all angles of attack'' published by International Journal of Micro Air Vehicles.

本风洞数据集采集于代尔夫特理工大学（TU Delft）的OJF设施。本数据集记录了经改装的MH32机翼在全攻角范围内，不同襟翼偏角以及0%、70%油门工况下的气动力与气动力矩。该数据集对尾座式飞行器（tailsitter）的相关研究具有重要参考价值，尤其可用于探究下降阶段逆流对尾座式飞行器的影响。
本数据集还补充提供了2021年2月24日采集的0%油门工况重复实验数据，用于验证测量结果的准确性。
本数据集关联发表于《国际微型飞行器期刊》（International Journal of Micro Air Vehicles）的论文《全攻角机翼风洞试验》。