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: 10.4121/16620226

Ma, Ziqing; Smeur, Ewoud (2022): Wind tunnel data set with a wing at all angles of attack. Version 3. 4TU.ResearchData. dataset. https://doi.org/10.4121/16620226.v3

Dataset

x choose version: version 2 - 2022-05-10 version 1 - 2022-01-07

• Aerospace Engineering

control effectiveness, inverse flow, tailsitter UAVs, wind tunnel test, wing-propeller interaction

February 24-26, 2021

CC0

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

by Ziqing Ma, Ewoud Smeur

This wind tunnel data set was collected at OJF in TU Delft. The aerodynamic forces and moments of a modified MH32 wing at all angles of attack for different flap deflections and 0%, 70% throttle settings are recorded in this data set. This data set should be valuable for the research on tailsitters, especially the impact of inverse flow on the tailsitters in the descending phase.

The repeated experiment data for 0% throttle on Feb 24, 2021 are also provided as a supplement to validate the accuracy of the measurements.

The dataset is related to the article ''Wind tunnel tests of a wing at all angles of attack'' published by International Journal of Micro Air Vehicles.

• 2022-01-07 first online

• 2022-07-19 published, posted

4TU.ResearchData

.txt files for readme and measurements

Wind tunnel tests of a wing at all angles of attack

TU Delft, Faculty of Aerospace Engineering