Wind Tunnel Research of Wingtip Devices

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F09%3A%230000901" target="_blank" >RIV/00010669:_____/09:#0000901 - 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

Wind Tunnel Research of Wingtip Devices

Original language description

Experimental model of straight higher-aspect ratio wing with eight different wingtips was studied at low-speed wind tunnel. Systematic study of wingtip influence provided fundamental experimental data concerning the possibilities to influence aerodynamiccharacteristics of wing by its wingtip devices, especially the characteristics difficult to compute. The data serve also for validation and setting of the calculation methods.

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

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2009

Confidentiality

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

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2/2009

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

7

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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