New Design of Whirl Flutter Aeroelastic Demonstrator
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F24%3AN0000044" target="_blank" >RIV/00010669:_____/24:N0000044 - isvavai.cz</a>
Výsledek na webu
<a href="https://conf.ifasd2024.nl/proceedings/display_manuscript/56.htm" target="_blank" >https://conf.ifasd2024.nl/proceedings/display_manuscript/56.htm</a>
DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
New Design of Whirl Flutter Aeroelastic Demonstrator
Popis výsledku v původním jazyce
This paper presents the new design of aeroelastic demonstrator for the experimental research into whirl flutter aeroelastic phenomenon. It represents a half-wing with the nacelle and powered propeller. In the frame of the previous project, two experimental campaigns were accomplished. For the further usage of the demonstrator, the modifications and upgrades were proposed. This paper presents the preparatory activities including the demonstrator design, instrumentation, and aerodynamic and structural analyses. Two experimental campaigns are planned in 2024 including the measurements of aerodynamic derivatives and measurements of dynamic response and whirl flutter stability.
Název v anglickém jazyce
New Design of Whirl Flutter Aeroelastic Demonstrator
Popis výsledku anglicky
This paper presents the new design of aeroelastic demonstrator for the experimental research into whirl flutter aeroelastic phenomenon. It represents a half-wing with the nacelle and powered propeller. In the frame of the previous project, two experimental campaigns were accomplished. For the further usage of the demonstrator, the modifications and upgrades were proposed. This paper presents the preparatory activities including the demonstrator design, instrumentation, and aerodynamic and structural analyses. Two experimental campaigns are planned in 2024 including the measurements of aerodynamic derivatives and measurements of dynamic response and whirl flutter stability.
Klasifikace
Druh
O - Ostatní výsledky
CEP obor
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OECD FORD obor
20304 - Aerospace engineering
Návaznosti výsledku
Projekt
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Návaznosti
R - Projekt Ramcoveho programu EK
Ostatní
Rok uplatnění
2024
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů