Low - speed wind tunnel testing for an unmanned aerial vehicle airfoil
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F09%3A00159911" target="_blank" >RIV/68407700:21220/09:00159911 - 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
Low - speed wind tunnel testing for an unmanned aerial vehicle airfoil
Original language description
This paper presents low speed wind tunnel tests of a 2D NACA airfoil which were performed by means of an aerodynamic measurement system. The lift, drag forces and pitching moment are shown. Finally, results of the wind tunnel tests were compared with references and found to be in good agreement.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2009
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Colloquiun Fluid Dynamics 2009 Proceedings
ISBN
978-80-87012-21-5
ISSN
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e-ISSN
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Number of pages
2
Pages from-to
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Publisher name
Institute of Thermomechanics, AS CR, v.v.i.
Place of publication
Prague
Event location
Praha
Event date
Oct 21, 2009
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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