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.

The dataset consists of the following measurement data:

Chordwise wing surface pressure distributions
Sectional aerodynamic polars of the wing in powered and unpowered configurations
Total pressure distributions in the wake of the wing
7-hole pressure probe measurements of various measurements planes around the wing, yielding static pressure, total pressure and velocity component distributions
Oil flow visualisations on both sides of the wing (qualitative)
Infrared Thermography (qualitative)

The full methodology, file description, naming convention, etc. are included in the attached README.

The wing model geometry is available from DOI: 10.5281/zenodo.13344026

The propeller geometry is available from DOI: 10.5281/zenodo.6355670