Poster-1: Fluid-Structure Coupling of Membrane Wings for improved MAV Performance

Published: 12 Dec 2016 | Version 1 | DOI: 10.17632/f53c73zyvb.1
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Description of this data

The poster shows details about some results from my PhD, involving experimental wind tunnel measurements on bio-inspired flexible wings for small drones, UAVs and MAVs.

Experiment data files

Steps to reproduce

-Experimental wind tunnel setup with rolling road and sting arm
-Load-cell + DIC + PIV equipment
-Processing and correlation of fluid-structure coupling phenomenons.

Related links

Latest version

  • Version 1

    2016-12-12

    Published: 2016-12-12

    DOI: 10.17632/f53c73zyvb.1

    Cite this dataset

    Bleischwitz, Robert; de Kat, Roeland; Ganapathisubramani, Bharathram (2016), “Poster-1: Fluid-Structure Coupling of Membrane Wings for improved MAV Performance”, Mendeley Data, v1 http://dx.doi.org/10.17632/f53c73zyvb.1

Statistics

Views: 57
Downloads: 16

Institutions

University of Southampton

Categories

3D Imaging, Aerodynamics, Unmanned Aerial Vehicle (Space Vehicle), Dynamic Loads, Deformation Analysis, Particle Image Velocimetry, Fluid-Structure Interaction

Licence

CC BY 4.0 Learn more

The files associated with this dataset are licensed under a Creative Commons Attribution 4.0 International licence.

What does this mean?

This dataset is licensed under a Creative Commons Attribution 4.0 International licence. What does this mean? You can share, copy and modify this dataset so long as you give appropriate credit, provide a link to the CC BY license, and indicate if changes were made, but you may not do so in a way that suggests the rights holder has endorsed you or your use of the dataset. Note that further permission may be required for any content within the dataset that is identified as belonging to a third party.

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