Flow Structure behind a Wing at High Reynolds Numbers
Institute of Thermomechanics, ASCR, v.v.i., Dolejškova 5, Praha 8, CR
2 UWB, Faculty of Mechanical Engineering, Department of Power System Engineering, Universitní 8, Plzeň, CR
3 VZLU, a. s., Beranových 130, Praha – Letňany, CR
* Corresponding author: email@example.com
Published online: 4 June 2018
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.
© The Authors, published by EDP Sciences, 2018
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