EXPERIMENTAL FLOW VISUALIZATION ALONG TWO-DIMENSIONAL AIRFOILS FOR AN UNMANNED AERIAL VEHICLE

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F10%3A00171966" target="_blank" >RIV/68407700:21220/10:00171966 - 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
EXPERIMENTAL FLOW VISUALIZATION ALONG TWO-DIMENSIONAL AIRFOILS FOR AN UNMANNED AERIAL VEHICLE
Popis výsledku v původním jazyce
This paper presents the collection of the fluid flow pattern images along a 2D NACA 2415 airfoil and four modifications of this one. Results allowed to obtain the location of the separation and reattachment point in some cases for different angles of attack by means of experimental visualization techniques such as oil and smoke. The experiments were held at a Reynolds number of 100000. Finally, experimental results were compared with numerical references and found in good agreement.
Název v anglickém jazyce
EXPERIMENTAL FLOW VISUALIZATION ALONG TWO-DIMENSIONAL AIRFOILS FOR AN UNMANNED AERIAL VEHICLE
Popis výsledku anglicky
This paper presents the collection of the fluid flow pattern images along a 2D NACA 2415 airfoil and four modifications of this one. Results allowed to obtain the location of the separation and reattachment point in some cases for different angles of attack by means of experimental visualization techniques such as oil and smoke. The experiments were held at a Reynolds number of 100000. Finally, experimental results were compared with numerical references and found in good agreement.

Rok uplatnění
2010
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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