cff-version: 1.2.0
abstract: "<p>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.</p><p><br></p><p>The dataset consists of the following measurement data:</p><ul><li>Chordwise wing surface pressure distributions</li><li>Sectional aerodynamic polars of the wing in powered and unpowered configurations</li><li>Total pressure distributions in the wake of the wing</li><li>7-hole pressure probe measurements of various measurements planes around the wing, yielding static pressure, total pressure and velocity component distributions</li><li>Oil flow visualisations on both sides of the wing (qualitative)</li><li>Infrared Thermography (qualitative)</li></ul><p><br></p><p>The full methodology, file description, naming convention, etc. are included in the attached README.</p><p><br></p><p>The wing model geometry is available from DOI: 10.5281/zenodo.13344026</p><p>The propeller geometry is available from DOI: 10.5281/zenodo.6355670</p>"
authors:
  - family-names: Duivenvoorden
    given-names: Ramon
    orcid: "https://orcid.org/0000-0002-3094-2782"
  - family-names: Sinnige
    given-names: Tomas
  - family-names: Veldhuis
    given-names: Leo
    orcid: "https://orcid.org/0000-0002-4869-8423"
title: "Experimental dataset of a single propeller-wing-flap model (TUD-PWF) at various flap deflections, angles of attack and propeller conditions"
keywords:
version: 1
identifiers:
  - type: doi
    value: 10.4121/3161b813-ad38-4f9c-bb9d-333b895f46bc.v1
license: CC BY-NC-ND 4.0
date-released: 2025-04-11