Grid Generation in ICEM CFD Software for CFD Calculation of Wing with High Lift Devices
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001021" target="_blank" >RIV/00010669:_____/10:#0001021 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Grid Generation in ICEM CFD Software for CFD Calculation of Wing with High Lift Devices
Original language description
This article deals with the grid creation for Euler and RANS computation of wing of airliner with high-lift devices in ANSYS ICEM CFD program. The pros and cons usage of tetrahedral and hexahedral grid are brought out. The problems which can appear during this process are mentioned and the possible solutions are presented.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Czech Aerospace Proceedings / Letecký zpravodaj
ISSN
1211-877X
e-ISSN
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Volume of the periodical
2/2010
Issue of the periodical within the volume
2
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
3
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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