Experimental Investigation an Numerical Analysis of Flow Past Airfoils with spoilers and High Lift Devices

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F10%3A00179167" target="_blank" >RIV/68407700:21220/10:00179167 - 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 Investigation an Numerical Analysis of Flow Past Airfoils with spoilers and High Lift Devices

Popis výsledku v původním jazyce

The paper focuses on airfoils with spoilers and high lift devices. The investigation was carried out using experimental and numerical methods. Results of two methods of visualization (Particle Image Velocimetry, Smoke wire) for three types of airfoils (with two different spoilers and split flap) were extended by pressure distribution measurement for one airfoil. The measurements were taken in open and closed circuit wind tunnels. Pressure distribution, velocity profile and images of flow in the airfoilvicinity were evaluated from numerical computations. The obtained data was prepared for mutual comparison and results were discussed.

Název v anglickém jazyce

Experimental Investigation an Numerical Analysis of Flow Past Airfoils with spoilers and High Lift Devices

Popis výsledku anglicky

The paper focuses on airfoils with spoilers and high lift devices. The investigation was carried out using experimental and numerical methods. Results of two methods of visualization (Particle Image Velocimetry, Smoke wire) for three types of airfoils (with two different spoilers and split flap) were extended by pressure distribution measurement for one airfoil. The measurements were taken in open and closed circuit wind tunnels. Pressure distribution, velocity profile and images of flow in the airfoilvicinity were evaluated from numerical computations. The obtained data was prepared for mutual comparison and results were discussed.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

BK - Mechanika tekutin

OECD FORD obor

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Projekt

Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2010

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Technical Soaring

ISSN

0744-8996

e-ISSN

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Svazek periodika

34

Číslo periodika v rámci svazku

4

Stát vydavatele periodika

NL - Nizozemsko

Počet stran výsledku

8

Strana od-do

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Kód UT WoS článku

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EID výsledku v databázi Scopus

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