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

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F12%3A00214340" target="_blank" >RIV/68407700:21220/12:00214340 - 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

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

Original language description

One of the possibility how to reduce cost of flying, is using various shapes of wing tips called winglets. To analyse these wing tips, it is useful, to develop objective method, which allows to compare aerodynamic characteristics of planar and nonplanarwing tips. This study 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, whichwas validated by experimental measurement provided by VZLU.

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

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2012

Confidentiality

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

Name of the periodical

Czech Aerospace

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2/2012

Issue of the periodical within the volume

2/2012

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

5-8

UT code for WoS article

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EID of the result in the Scopus database

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