UNSTEADY MEASUREMENTS OF AERODYNAMIC CHARACTERISTICS OF THE AIRFOIL

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F10%3A00424903" target="_blank" >RIV/60162694:G43__/10:00424903 - 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
UNSTEADY MEASUREMENTS OF AERODYNAMIC CHARACTERISTICS OF THE AIRFOIL
Original language description
This paper deals with unsteady measurements of aerodynamic characteristics of the symmetric airfoil for the angle of attack within the range from 0° to 360° with variable value of angular velocity. These results are processed for first and second revolution of airfoil. For these tests was designed a special device. Key words: unsteady aerodynamic, load and pressure unsteady measurement of airfoil, Dynamic Stall.
Czech name
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Czech description
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Project
<a href="/en/project/GAP101%2F10%2F0257" target="_blank" >GAP101/10/0257: Influence of Heat Transfer on Laminar-Turbulent Transition</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
PROCEEDINGS OF THE 9TH INTERNATIONAL SCIENTIFIC CONFERENCE NEW TRENDS IN AVIATION DEVELOPMENT
ISBN
978-80-553-0475-5
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
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Publisher name
Technická univerzita Košice
Place of publication
Prešov
Event location
GERLACHOV - HIGH TATRAS
Event date
Jan 1, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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