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/d0521ec8-a349-45ea-80a6-905102055c9a

Zoppini, Giulia (2023): Data underlying the PhD thesis: Receptivity of Swept Wing Boundary Layers to Surface Roughness. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/d0521ec8-a349-45ea-80a6-905102055c9a.v1

Dataset

• Aerospace Engineering
• Engineering

bounday layer, crossflow, fluid dynamics, instability, transition

CC BY 4.0

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Giulia Zoppini

3 Sets of data were acquired from different experimental measurements dedicated to characterising the boundary layer of a swept wing dominated by crossflow instabilities. The Planar_PIV folder contains data acquired with planar PIV and describes the boundary layer spanwise and wall-normal velocity components at various chord locations. The HWA folder contains hot wire anemometry acquisition measuring the velocity fields in the spanwise and wall-normal direction. These fields are acquired in the vicinity of a roughness element. The Planar_PIV_control folder contains planar PIV fields describing the boundary layer spanwise and wall-normal velocity components at various chord locations in the presence of passive flow control on the wing. All folders are accompanied by thermal images acquired through infrared thermography, which provide the global boundary layer behaviour (i.e. laminar or turbulent state). More info on data acquisition and processing can be found in the corresponding PhD Thesis.

• 2023-04-12 first online, published, posted

4TU.ResearchData

.mat files organized in .zip folders

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