Published December 5, 2024 | Version v1

Data from: Highly deformable flapping membrane wings suppress the leading edge vortex in hover to perform better

  • 1. École Polytechnique Fédérale de Lausanne
  • 2. ROR icon Brown University

Description

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: https://doi.org/10.1073/pnas.2410833121

Files

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Additional details

Related works

Is published in
Journal article: 10.1073/pnas.2410833121 (DOI)

Funding

Swiss National Science Foundation
Reconfigurable airfoil shape and orientation for improved performance during stroke and flow reversal 200021_175792

Software

Programming language
MATLAB