The doi 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: 10.4121/0b01a240-559f-4f4b-802d-7b1d36aa0024

Xu, Guanqun; Yu, Wei; Andrea Sciacchitano; Simao Ferreira, Carlos; Iyer, Sowmya (2024): Data from the study of PIV measurement flow field of the airfoil NACA0021 under surging motion. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/0b01a240-559f-4f4b-802d-7b1d36aa0024.v1

Dataset

• Aerospace Engineering
• Engineering

airfoil surging, large angles of attack, Particle Image Velocimetry, PIV, Vortex-induced vibration

CC BY 4.0

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by Guanqun Xu , Wei Yu , Andrea Sciacchitano , Carlos Simao Ferreira , Sowmya Iyer

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. The main goal is to investigate the vortex structures from formation and evolution to shedding and their role in the aerodynamic forces. This experimental dataset contains particle image velocimetry (PIV) measurements of the flow field velocity around a NACA0021 airfoil undergoing surging motion at two different frequencies (reduced frequency k = 0.19 and k = 0.38). The dataset includes dynamic (surging) cases and a static case for comparison.

• 2024-10-25 first online, published, posted

4TU.ResearchData

mat, gif

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