Data underlying the publication: An experimental study of the unsteady aerodynamics of a static DU91-W2-150 airfoil at large angles of attack

DOI:10.4121/c42b2fe5-5df6-4518-ab26-604502f311cc.v1
The DOI displayed above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
DOI: 10.4121/c42b2fe5-5df6-4518-ab26-604502f311cc
Datacite citation style:
Xu, Guanqun; Yu, Wei; Andrea Sciacchitano; Carlos Ferreira (2024): Data underlying the publication: An experimental study of the unsteady aerodynamics of a static DU91-W2-150 airfoil at large angles of attack. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/c42b2fe5-5df6-4518-ab26-604502f311cc.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite

Dataset

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.

History

  • 2024-12-31 first online, published, posted

Publisher

4TU.ResearchData

Format

txt, xlsx

Organizations

TU Delft, Faculty of Aerospace Engineering, Department of Flow Physics and Technology

DATA

Files (1)