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

Kód výsledku v 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>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

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

Popis výsledku v původním jazyce

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.

Název v anglickém jazyce

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

Popis výsledku anglicky

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.

Druh

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

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2012

Kód důvěrnosti údajů

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

Název periodika

Czech Aerospace

ISSN

1211-877X

e-ISSN

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Svazek periodika

2/2012

Číslo periodika v rámci svazku

2/2012

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

4

Strana od-do

5-8

Kód UT WoS článku

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EID výsledku v databázi Scopus

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