Experimental and computational study of ground effect on airfoil section

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F16%3AN0000103" target="_blank" >RIV/00010669:_____/16:N0000103 - isvavai.cz</a>
Výsledek na webu
<a href="http://icas.org/ICAS_ARCHIVE/ICAS2016/data/papers/2016_0122_paper.pdf" target="_blank" >http://icas.org/ICAS_ARCHIVE/ICAS2016/data/papers/2016_0122_paper.pdf</a>
DOI - Digital Object Identifier
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Jazyk výsledku
angličtina
Název v původním jazyce
Experimental and computational study of ground effect on airfoil section
Popis výsledku v původním jazyce
The influence of ground proximity on aerodynamic characteristics of an airfoil was studied at low Reynolds number. The study, motivated mainly by sailplane take-off and landing safety, provides information about the development of the pressure distributions and of the aerodynamic forces acting on the airfoil with the approaching of the airfoil to the ground. Differences caused by fixed or by moving ground were examined using CFD computations.
Název v anglickém jazyce
Experimental and computational study of ground effect on airfoil section
Popis výsledku anglicky
The influence of ground proximity on aerodynamic characteristics of an airfoil was studied at low Reynolds number. The study, motivated mainly by sailplane take-off and landing safety, provides information about the development of the pressure distributions and of the aerodynamic forces acting on the airfoil with the approaching of the airfoil to the ground. Differences caused by fixed or by moving ground were examined using CFD computations.

Projekt
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Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění
2016
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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