Numerical Investigation of Aeroelastic Flutter in Two-Dimensional Cascade of Compressor Blades
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24220%2F20%3A00008041" target="_blank" >RIV/46747885:24220/20:00008041 - 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
Numerical Investigation of Aeroelastic Flutter in Two-Dimensional Cascade of Compressor Blades
Original language description
There are two major areas of applied aerodynamics research where flutter occurrence plays important role. The first one is aircraft industry with strict requirements of safety resulting in careful wing design preventing any kind of dynamic instability. The second one is gas turbine engines where jet-engine companies keep pushing the limits of efficiency and performance.
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
10102 - Applied mathematics
Result continuities
Project
<a href="/en/project/GA20-11537S" target="_blank" >GA20-11537S: Experimental research on flutter excitation function in turbomachinery</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>S - Specificky vyzkum na vysokych skolach
Others
Publication year
2020
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů