New Design of Whirl Flutter Aeroelastic Demonstrator
The result's identifiers
Result code in 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>
Result on the web
<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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Alternative languages
Result language
angličtina
Original language name
New Design of Whirl Flutter Aeroelastic Demonstrator
Original language description
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.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
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Continuities
R - Projekt Ramcoveho programu EK
Others
Publication year
2024
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů