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

Result code in 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>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

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

Original language description

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.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

BK - Liquid mechanics

OECD FORD branch

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Project

Result was created during the realization of more than one project. More information in the Projects tab.

Continuities

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

Publication year

2010

Confidentiality

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

Name of the periodical

Technical Soaring

ISSN

0744-8996

e-ISSN

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Volume of the periodical

34

Issue of the periodical within the volume

4

Country of publishing house

NL - THE KINGDOM OF THE NETHERLANDS

Number of pages

8

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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