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