Flow Structure behind a Wing at High Reynolds Numbers
- Uruba Václav
- Pátek Zdeněk
- Procházka Pavel
- Skála Vladislav
- Zacho David
- Kulhánek Robert
Publication date
January 2018
DOI Publisher
EDP Sciences ISSN
2100-014X Journal
EPJ Web of Conferences Citation count (estimate)
1Abstract
The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to study the vortical structures oriented in the streamwise direction, which take place both in suction and pressure sides of the wing. The Reynolds numbers during the experiments in the 3 m wind tunnel range from 0.5 million up to 1.5 million
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