Ma, Ziqing; Smeur, Ewoud (2022): Wind tunnel data set with a wing at all angles of attack. Version 2. 4TU.ResearchData. dataset. https://doi.org/10.4121/16620226.v2

Dataset

x choose version: version 3 - 2022-07-19 (latest) 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.

• 2022-01-07 first online

• 2022-05-10 published, posted

4TU.ResearchData

.txt files for readme and measurements

TU Delft, Faculty of Aerospace Engineering