Flutter boundary assessment for a blade cascade using developed discontinuous Galerkin code
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23520%2F18%3A43953260" target="_blank" >RIV/49777513:23520/18:43953260 - 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
Flutter boundary assessment for a blade cascade using developed discontinuous Galerkin code
Original language description
The target of this contribution is to introduce a fluid-structure interaction (FSI) code developed for the purpose of the flutter analysis in a blade cascade. The algorithm is based on the discretisation of the system of Navier-Stokes equations by the discontinuous Galerkin method. The results produced by the FSI code are benchmarked against published results of the flutter boundary assessment for a single wing. Furthermore, the FSI code is applied to the prediction of flutter boundary in a blade cascade.
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
20302 - Applied mechanics
Result continuities
Project
<a href="/en/project/GA16-04546S" target="_blank" >GA16-04546S: Aero-elastic couplings and dynamic behaviour of rotational periodic bodies</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů