The solution of the flow field around the wing with a focuse on the induced effects

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F12%3A00214640" target="_blank" >RIV/68407700:21220/12:00214640 - isvavai.cz</a>
Výsledek na webu
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DOI - Digital Object Identifier
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Jazyk výsledku
angličtina
Název v původním jazyce
The solution of the flow field around the wing with a focuse on the induced effects
Popis výsledku v původním jazyce
One of the possibility how to reduce costs of flying, is using various shapes of wing tips. To analyse these wing tips, it is useful, to develop objective method, which allows to compare aerodynamic characteristics of planar and nonplanar wing tips. Thisstudy was especially focused on the wing tips in the category of Light Sport Aircraft (LSA), where the research was not done sufficiently yet. The solving of the flow field around the wing was resolved by using numerical simulation, which was validatedby experimental measurement provided by VZLU.
Název v anglickém jazyce
The solution of the flow field around the wing with a focuse on the induced effects
Popis výsledku anglicky
One of the possibility how to reduce costs of flying, is using various shapes of wing tips. To analyse these wing tips, it is useful, to develop objective method, which allows to compare aerodynamic characteristics of planar and nonplanar wing tips. Thisstudy was especially focused on the wing tips in the category of Light Sport Aircraft (LSA), where the research was not done sufficiently yet. The solving of the flow field around the wing was resolved by using numerical simulation, which was validatedby experimental measurement provided by VZLU.

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

Rok uplatnění
2012
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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