Data from: Highly deformable flapping membrane wings suppress the leading edge vortex in hover to perform better
This directory contains open-source data obtained at the UNFOLD laboratory at EPFL. The data got recorded for the flexible membrane wings with different stiffnesses expressed by the aeroelastic number Ae and recorded at different angles of attack.
More information about the study can be found at:
-coming soon, once DOI is assigned by journal-
1235a61f-cd69-4a38-a17e-6bff8b35c932
École Polytechnique Fédérale de Lausanne ; Brown University
EPFL
2024-12-05
1
CC BY
| Funder | Funding(s) | Grant NO | Grant URL |
Swiss National Science Foundation | Reconfigurable airfoil shape and orientation for improved performance during stroke and flow reversal | 200021_175792 | |
| Relation | Related work | URL/DOI |
IsVersionOf | ||
IsSupplementTo | Highly deformable flapping membrane wings suppress the leading edge vortex in hover to perform better | |