The DOI displayed 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: 10.4121/8b78a204-e41e-4ec3-ae5d-dbb8df7f8922

Ma, Ziqing; Smeur, Ewoud (2025): Wind tunnel test dataset of a tilt-rotor tailsitter focusing on wing-propeller interaction. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/8b78a204-e41e-4ec3-ae5d-dbb8df7f8922.v1

Categories

• Aerospace Engineering
• Engineering

Keywords

Aerodynamics Control surfaces tailsitter UAVs Tilt rotor Unmanned Aerial Vehicle (UAV) wind tunnel data wing-propeller interaction

Geolocation

Time coverage

Jan 2025, April 2025

Licence

CC BY 4.0

Interoperability

• RO-Crate Metadata

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by Ziqing Ma , Ewoud Smeur

This wind tunnel data set was collected at OJF in TU Delft. This dateset records the static measured aerodynamic forces and moments of a customized tilt-rotor tailsitter at all angles of attack for different rotor tilt angle, thrust throttle, elevon defletion, airspeed and angle of attack, and also includes data recorded during a realtime dynamic moment trim test. This data set should be valuable for the research on tailsitters, especially the impact of wing-propeller interaction.

History

• 2025-07-18 first online, published, posted

Publisher

4TU.ResearchData

Format

MATLAB/.m, ROS/.bag, image/.jpg

Organizations

TU Delft, Faculty of Aerospace Engineering, Department of Control and Operations, Control and Simulation