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-