Comparison of CFD Methods Applied on Vilik Flying Model

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001020" target="_blank" >RIV/00010669:_____/10:#0001020 - 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

Comparison of CFD Methods Applied on Vilik Flying Model

Popis výsledku v původním jazyce

One of the tasks of the research project was to perform complete aerodynamic analysis on radio control model Vilik. For these purposes, extensive wind tunnel tests and computations with usage of panel and CFD methods have been performed. This article deals with the comparison of programmes Edge and Star CCM+ used for calculations. As results lift curves, moment and polar curves have been established, and consequently further aerodynamic characteristics for sideslip flight and regimes with various deflections of ailerons and tails have been analyzed. The results were used for simulation of a fully nonlinear mathematical model of aircraft motion, which was a significant task of the research project.

Název v anglickém jazyce

Comparison of CFD Methods Applied on Vilik Flying Model

Popis výsledku anglicky

One of the tasks of the research project was to perform complete aerodynamic analysis on radio control model Vilik. For these purposes, extensive wind tunnel tests and computations with usage of panel and CFD methods have been performed. This article deals with the comparison of programmes Edge and Star CCM+ used for calculations. As results lift curves, moment and polar curves have been established, and consequently further aerodynamic characteristics for sideslip flight and regimes with various deflections of ailerons and tails have been analyzed. The results were used for simulation of a fully nonlinear mathematical model of aircraft motion, which was a significant task of the research project.

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

Z - Vyzkumny zamer (s odkazem do CEZ)

Rok uplatnění

2010

Kód důvěrnosti údajů

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

Název periodika

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Svazek periodika

4/2010

Číslo periodika v rámci svazku

4

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

4

Strana od-do

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Kód UT WoS článku

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EID výsledku v databázi Scopus

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