The solution of the flow field around the wing with a focuse on the induced effects
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F12%3A00214640" target="_blank" >RIV/68407700:21220/12:00214640 - 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
The solution of the flow field around the wing with a focuse on the induced effects
Original language description
One of the possibility how to reduce costs of flying, is using various shapes of wing tips. To analyse these wing tips, it is useful, to develop objective method, which allows to compare aerodynamic characteristics of planar and nonplanar wing tips. Thisstudy 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, which was validatedby experimental measurement provided by VZLU.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
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
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
READ 2012
ISBN
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ISSN
1425-2104
e-ISSN
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Number of pages
10
Pages from-to
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Publisher name
VUT v Brně
Place of publication
Brno
Event location
Brno
Event date
Oct 17, 2012
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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