cff-version: 1.2.0
abstract: "<p>The main goal of this research is to experimentally investigate the unsteady aerodynamics of a static airfoil at large angles of attack (AoA), with a focus on the wake flow dynamics, vortex shedding characteristics and airfoil loading. This dataset contains the experimental measurement of a static DU91-W2-150 airfoil in a closed wind tunnel. This experimental study tested the airfoil under a wide range of AoA from 0◦ to 310◦ at three Reynolds numbers (Re) from 2×10^5 to 8×10^5. Pressure on the airfoil surface was measured and Particle Image Velocimetry (PIV) measurements were conducted to capture the flow field in the wake.</p>"
authors:
  - family-names: Xu
    given-names: Guanqun
    orcid: "https://orcid.org/0000-0002-8520-3055"
  - family-names: Yu
    given-names: Wei
    orcid: "https://orcid.org/0000-0001-7829-6129"
  - family-names: Sciacchitano
    given-names: Andrea
    orcid: "https://orcid.org/0000-0003-4627-3787"
  - family-names: Ferreira
    given-names: Carlos
    orcid: "https://orcid.org/0000-0003-0192-3651"
title: "Data underlying the publication: An experimental study of the unsteady aerodynamics of a static DU91-W2-150 airfoil at large angles of attack"
keywords:
version: 1
identifiers:
  - type: doi
    value: 10.4121/c42b2fe5-5df6-4518-ab26-604502f311cc.v1
license: CC BY 4.0
date-released: 2024-12-31