Please use this identifier to cite or link to this item: https://doi.org/10.15480/882.3288
Publisher DOI: 10.1007/s11071-020-06171-8
Title: Spatially localized vibrations in a rotor subjected to flutter
Language: English
Authors: Nitti, Alessandro 
Stender, Merten  
Hoffmann, Norbert  
Papangelo, Antonio 
Keywords: Airfoil;Basin stability;Flutter;Geometrical nonlinearity;Localized vibrations
Issue Date: 11-Jan-2021
Publisher: Springer Science + Business Media B.V
Source: Nonlinear Dynamics 1 (103): 309-325 (2021-01-11)
Journal or Series Name: Nonlinear dynamics 
Abstract (english): 
The current push toward lightweight structures in aerospace and aeronautical engineering is leading to slender design airfoils, which are more likely to undergo large deformation, hence experiencing geometrical nonlinearities. The problem of vibration localization in a rotor constituted by N coupled airfoils with plunge and pitch degrees of freedom subjected to flutter instability is considered. For a single airfoil, it is shown that depending on the system parameters, multiple static and dynamic equilibria coexist which may be a fixed point, a limit cycle, or irregular motion. By elastically coupling N airfoils, a simplified rotor model is obtained. The nonlinear dynamical response of the rotor is studied via time integration with particular attention to the emergence of localized vibrating solutions, which have been classified introducing a localization coefficient. Finally, the concept of basin stability is exploited to ascertain the likelihood of the system to converge to a certain localized state as a function of the airstream velocity. We found that homogeneous and slightly localized states are more likely to appear with respect to strongly localized states.
URI: http://hdl.handle.net/11420/8774
DOI: 10.15480/882.3288
ISSN: 1573-269X
Institute: Strukturdynamik M-14 
Document Type: Article
Funded by: Open Access funding enabled and organized by Projekt DEAL. M.S. was supported by the German Research Foundation (DFG) within the Priority Program ’calm, smooth, smart’ under the reference Ho 3851/121. A.P. acknowledges the DFG (German Research Foundation) for funding the project PA 3303/1-1. A.P. acknowledges support from PON Ricerca e Innovazione 2014-2020-Azione I.2 - D.D. n. 407, 27/02/2018, bando AIM (Grant No. AIM1895471). A.P. acknowledges the support by the Italian Ministry of Education, University and Research under the Programme Department of Excellence Legge 232/2016 (Grant No. CUP-D94I18000260001).
License: CC BY 4.0 (Attribution) CC BY 4.0 (Attribution)
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