Wind tunnel tests of oscillating wing using the surface pressure transducers.

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230000998" target="_blank" >RIV/00010669:_____/10:#0000998 - isvavai.cz</a>
Výsledek na webu
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DOI - Digital Object Identifier
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Jazyk výsledku
angličtina
Název v původním jazyce
Wind tunnel tests of oscillating wing using the surface pressure transducers.
Popis výsledku v původním jazyce
This article deals with aerodynamic measurement of oscillated wing model AS28 with newly installed surface pressure transducers KULITE. In the frame of this work the practical task of the test of new technology of the surface pressure measurement and verifying of early results measured on this model was realized. There is introduced the development of unsteady measurement on the oscillated half-wing model in high speed laboratory of VZLU, the measurement, results and comparison of used methods.
Název v anglickém jazyce
Wind tunnel tests of oscillating wing using the surface pressure transducers.
Popis výsledku anglicky
This article deals with aerodynamic measurement of oscillated wing model AS28 with newly installed surface pressure transducers KULITE. In the frame of this work the practical task of the test of new technology of the surface pressure measurement and verifying of early results measured on this model was realized. There is introduced the development of unsteady measurement on the oscillated half-wing model in high speed laboratory of VZLU, the measurement, results and comparison of used methods.

Druh
J<sub>x</sub> - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
CEP obor
JU - Aeronautika, aerodynamika, letadla
OECD FORD obor
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Rok uplatnění
2010
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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