Flow Structure behind a Wing at High Reynolds Numbers

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000080" target="_blank" >RIV/00010669:_____/18:N0000080 - isvavai.cz</a>
Alternative codes found
RIV/61388998:_____/18:00498477 RIV/49777513:23210/18:43954518
Result on the web
<a href="https://www.epj-conferences.org/articles/epjconf/abs/2018/15/epjconf_efm2018_02111/epjconf_efm2018_02111.html" target="_blank" >https://www.epj-conferences.org/articles/epjconf/abs/2018/15/epjconf_efm2018_02111/epjconf_efm2018_02111.html</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/epjconf/201818002111" target="_blank" >10.1051/epjconf/201818002111</a>

Result language
angličtina
Original language name
Flow Structure behind a Wing at High Reynolds Numbers
Original language description
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.
Czech name
—
Czech description
—

Project
<a href="/en/project/GA17-01088S" target="_blank" >GA17-01088S: 3D Instability of a Shear Layer in Adverse Pressure Gradient</a><br>
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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