Gai, Guanqun and Timme, Sebastian ORCID: 0000-0002-2409-1686
(2016)
Nonlinear reduced-order modelling for limit-cycle oscillation analysis.
Nonlinear Dynamics, 84 (2).
pp. 991-1009.
Text
gai2015.pdf - Unspecified Access to this file is embargoed until Unspecified. Download (1MB) |
Abstract
A nonlinear model reduction based on eigenmode decomposition and projection for the prediction of sub- and supercritical limit-cycle oscillation is presented herein. The paper focuses on the derivation of the reduced-order model formulation to include expansion terms up to fifth order such that higher-order nonlinear behaviour of a physical system can be captured. The method is applied to a two degree-of-freedom pitch–plunge aerofoil structural model in unsteady incompressible flow. Structural stiffness nonlinearity is introduced as a fifth-order polynomial, while the aerodynamics follow linear theory. It is demonstrated that the reduced-order model is capable of accurately capturing sub- and supercritical limit-cycle oscillations arising both from initial disturbances and gust excitation. Furthermore, an analysis of the computational cost associated with constructing such reduced-order model and its applicability to more complex aeroelastic problems is given.
Item Type: | Article |
---|---|
Uncontrolled Keywords: | Hopf bifurcation, Nonlinear model reduction, Eigenmode decomposition, Polynomial stiffness, Limit-cycle oscillation |
Subjects: | ?? TA ?? |
Depositing User: | Symplectic Admin |
Date Deposited: | 21 Jan 2016 09:32 |
Last Modified: | 09 Mar 2023 07:43 |
DOI: | 10.1007/s11071-015-2544-9 |
Related URLs: | |
URI: | https://livrepository.liverpool.ac.uk/id/eprint/2046062 |