Dynamic phenomena of a blade system with aero-elastic coupling
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23520%2F16%3A43929229" target="_blank" >RIV/49777513:23520/16:43929229 - 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
Dynamic phenomena of a blade system with aero-elastic coupling
Original language description
The paper presents an approach to bladed disk with aero-elastic coupling modelling. The bladed disk is created by blades modelled as airfoil profiles, which are mutually interconnected by shrouding. The shrouding and its parameters can along with the fluid flow velocity significantly decide on the stability of the complete system. Based on the performed analysis the mechanism of step by step switching between different kind of instabilities and stable regions is explained using a test bladed disk model.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BI - Acoustics and oscillation
OECD FORD branch
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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
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Proceedings of ISMA 2016 - USD 2016
ISBN
978-90-73802-91-9
ISSN
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e-ISSN
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Number of pages
8
Pages from-to
423-430
Publisher name
KU Leuven
Place of publication
Leuven
Event location
Leuven, Belgie
Event date
Sep 19, 2016
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000392486300034