Comparison of CFD Methods Applied on Vilik Flying Model

Result code in 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>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Comparison of CFD Methods Applied on Vilik Flying Model

Original language description

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.

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

2010

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

4/2010

Issue of the periodical within the volume

4

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

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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