Experimental dataset of a single propeller-wing-flap model (TUD-PWF) at various flap deflections, angles of attack and propeller conditions

Experimental dataset of wind tunnel campaigns with a propeller-wing-flap model, for the purpose of numerical validation or flow analysis. Acquired at the Low Turbulence Tunnel of the Delft University of Technology between 2021 and 2024.<br>The dataset consists of the following measurement data:Chordwise wing surface pressure distributionsSectional aerodynamic polars of the wing in powered and unpowered configurationsTotal pressure distributions in the wake of the wing7-hole pressure probe measurements of various measurements planes around the wing, yielding static pressure, total pressure and velocity component distributionsOil flow visualisations on both sides of the wing (qualitative)Infrared Thermography (qualitative)<br>The full methodology, file description, naming convention, etc. are included in the attached README.<br>The wing model geometry is available from DOI: 10.5281/zenodo.13344026The propeller geometry is available from DOI: 10.5281/zenodo.6355670

本数据集为螺旋桨-机翼-襟翼模型风洞试验数据集，旨在用于数值验证或流动分析。该数据集于2021年至2024年间在代尔夫特理工大学低湍流风洞（Low Turbulence Tunnel）采集完成。
数据集包含如下测量数据：
- 机翼表面沿弦向的压力分布；
- 带动力与无动力构型下的机翼截面气动极曲线；
- 机翼尾流区总压分布；
- 针对机翼周边多个测量平面的七孔压力探针（7-hole pressure probe）测量，可获取静压、总压与速度分量分布；
- 机翼两侧的油流可视化结果（定性）；
- 红外热成像（Infrared Thermography）结果（定性）。
完整的试验方法、文件说明与命名规范等内容均包含在附带的README文件中。
机翼模型几何参数可从DOI：10.5281/zenodo.13344026获取；螺旋桨几何参数可从DOI：10.5281/zenodo.6355670获取。