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: 10.4121/8cec2ee4-9dfa-47ba-a71d-69e73b625d38

Xu, Guanqun; Yu, Wei; Andrea Sciacchitano; Carlos Ferreira; Slooter, Pepijn (2024): Data from the pressure measurement of a pitching airfoil NACA643418. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/8cec2ee4-9dfa-47ba-a71d-69e73b625d38.v1

Categories

• Aerospace Engineering
• Engineering

Keywords

airfoil pitching dynamic stall large angles of attack pressure measurement Vortex-induced vibration

Licence

CC BY 4.0

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by Guanqun Xu , Wei Yu , Andrea Sciacchitano , Carlos Ferreira , Pepijn Slooter

The present experimental work is motivated by the need for additional insight into the vortex-induced vibrations (VIV) of airfoils at high angle of attack from an aerodynamic perspective. Airfoil NACA643418 is set to periodic pitching motion. This experimental dataset temporarily contains surface pressure measurements of a pitching airfoil with a mean angle of attack set at 170 degrees, pitching frequency of 2 Hz, and pitching amplitude of 1o degrees.

History

• 2024-11-15 first online, published, posted

Publisher

4TU.ResearchData

Format

mat, m

Organizations

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