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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

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

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Categories

• Aerospace Engineering

Keywords

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

Geolocation

Time coverage

February 24-26, 2021

Licence

CC0

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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.

History

• 2022-01-07 first online

• 2022-07-19 published, posted

Publisher

4TU.ResearchData

Format

.txt files for readme and measurements

Associated peer-reviewed publication

Wind tunnel tests of a wing at all angles of attack

Organizations

TU Delft, Faculty of Aerospace Engineering