Comparison of Aerodynamic Data Provided by Computation and Wind-Tunnel Testing
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F11%3A%230001188" target="_blank" >RIV/00010669:_____/11:#0001188 - isvavai.cz</a>
Result on the web
<a href="http://www.czaerospace.eu/en/2011-3-42.html" target="_blank" >http://www.czaerospace.eu/en/2011-3-42.html</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Comparison of Aerodynamic Data Provided by Computation and Wind-Tunnel Testing
Original language description
This article describes various computational and experimental methods for obtaining the aerodynamic characteristics of aircraft. These are used for development and verification software solutions for the dynamics and stability of fully non-linear mathematical model of aircraft movements.
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
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2011
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
3/2011
Issue of the periodical within the volume
3
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
5
Pages from-to
29-33
UT code for WoS article
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EID of the result in the Scopus database
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