Anisotropy of Turbulent Flow around an Airfoil
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23210%2F19%3A43960366" target="_blank" >RIV/49777513:23210/19:43960366 - isvavai.cz</a>
Alternative codes found
RIV/61388998:_____/19:00518668
Result on the web
<a href="https://www.engmech.cz/improc/2019/089_Uruba_142.pdf" target="_blank" >https://www.engmech.cz/improc/2019/089_Uruba_142.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.21495/71-0-379" target="_blank" >10.21495/71-0-379</a>
Alternative languages
Result language
angličtina
Original language name
Anisotropy of Turbulent Flow around an Airfoil
Original language description
The flow around an airfoil is analyzed from the point of view turbulence anisotropy assessment. The turbulent flow-field in the vicinity of an airfoil is populated by vortices, in some locations they tend to regularity in orientation, i.e. to anisotropy. However in the wake behind the plate as well as in the core of the boundary layer on the plate suction side the turbulence is close to isotropic state.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20302 - Applied mechanics
Result continuities
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
Others
Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
ENGINEERING MECHANICS 2019
ISBN
978-80-87012-71-0
ISSN
1805-8248
e-ISSN
1805-8256
Number of pages
4
Pages from-to
379-382
Publisher name
2019 Institute of Thermomechanics of the Czech Academy of Sciences, Prague
Place of publication
Praha
Event location
Svratka
Event date
May 13, 2019
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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