Structure of the Wake Behind an Airfoil

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23210%2F19%3A43960365" target="_blank" >RIV/49777513:23210/19:43960365 - isvavai.cz</a>
Alternative codes found
RIV/61388998:_____/19:00503320
Result on the web
<a href="https://www.researchgate.net/profile/Vaclav_Uruba/publication/331725077_STRUCTURE_OF_THE_WAKE_BEHIND_AN_AIRFOIL/links/5c8fd011299bf14e7e84aa60/STRUCTURE-OF-THE-WAKE-BEHIND-AN-AIRFOIL.pdf" target="_blank" >https://www.researchgate.net/profile/Vaclav_Uruba/publication/331725077_STRUCTURE_OF_THE_WAKE_BEHIND_AN_AIRFOIL/links/5c8fd011299bf14e7e84aa60/STRUCTURE-OF-THE-WAKE-BEHIND-AN-AIRFOIL.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.14311/TPFM.2019.026" target="_blank" >10.14311/TPFM.2019.026</a>

Result language
angličtina
Original language name
Structure of the Wake Behind an Airfoil
Original language description
The wake behind an inclined plate simulating airfoil is to be studied experimentally. The vortical structures are identified eventually. Theirs topology and dynamical behaviour is to be studied in details using the Proper Orthogonal Decomposition method. The stereo time resolved Particle Image Velocimetry technique is used for the experimental research. The vortex trains with oblique orientation and chequered topology have been detected.
Czech name
—
Czech description
—

Project
<a href="/en/project/LQ1603" target="_blank" >LQ1603: Research for SUSEN</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>S - Specificky vyzkum na vysokych skolach

Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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