Large-scale flow visualization of a flapping-wing micro air vehicle

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

24 Downloads (Pure)

Abstract

The aim of this investigation is to provide an experimental volumetric visualization of the near wake topology of the vortex structures generated by a flapping-wing Micro Air Vehicle (MAV) by means of large-scale Robotic PIV. This novel technique implements coaxial illumination and imaging in combination with the use of Helium Filled Soap Bubbles (HFSB) as tracing particles to achieve large measurement volumes of the order of 10 liters. Information of different phases throughout the flapping cycle is obtained by means of a phase-locked averaging procedure. Experiments in both tethered and free-flight conditions have been performed, yielding an unprecedented comparison between the aerodynamics of the two conditions.
Original languageEnglish
Title of host publicationProceedings 18th International Symposium on Flow Visualization
Subtitle of host publicationZurich, Switzerland, June 26-29, 2018
EditorsThomas Rösgen
PublisherETH Zürich
Number of pages20
DOIs
Publication statusPublished - 2018
EventISFV18: 18th International Symposium on Flow Visualization - Zürich, Switzerland
Duration: 26 Jun 201829 Jun 2018
Conference number: 18
http://www.isfv18.ethz.ch/

Conference

ConferenceISFV18: 18th International Symposium on Flow Visualization
Abbreviated titleISFV18
Country/TerritorySwitzerland
CityZürich
Period26/06/1829/06/18
Internet address

Fingerprint

Dive into the research topics of 'Large-scale flow visualization of a flapping-wing micro air vehicle'. Together they form a unique fingerprint.

Cite this