The objective of this paper is to present an analytical/numerical analysis of the phenomenon of limit-cycle stability reversal (from unstable to stable, and vice versa). A singular perturbation technique, the method of the normal form (in the asymptoticexpansion version), is utilized. The number of
WAVELET ANALYSIS FOR HOPF BIFURCATIONS WITH AEROELASTIC APPLICATIONS
โ Scribed by F. MASTRODDI; A. BETTOLI
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 411 KB
- Volume
- 225
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
A wavelet analysis on the output signal of a non-linear system in the neighbourhood of a Hopf bifurcation (i.e., a limit-cycle oscillation) has been performed to point out the linear and non-linear signatures of the system. Indeed, this kind of non-linear behaviour is characterized not only by a simple harmonic oscillation in developed steady state condition, but also by an initial transitory phase with a complex time evolution of the spectral signal content. Both these issues could be described in an analytical way via a singular perturbation analysis but they could be also directly analyzed by a signal-processing tool via wavelet analysis (Continuous Wavelet Transform, CWT): this is obtained by using the wavelet capability in describing e$ciently the time evolution of the spectrum of the signal (i.e., a non-linear &&signature'' of a Hopf bifurcation). Furthermore, the analytical results given by the singular perturbation analysis for the same class of non-linear problems, have allowed one to interpret correctly the results obtained by the wavelet analysis. In this paper this theoretical link between the wavelet analysis and the output signal of a dynamical system (recently achieved for linear mechanical damped systems) has been extended to non-linear systems in the neighbourhood of a Hopf bifurcation. This kind of analysis is of natural interest in aeroelastic applications where an e$cient (and noise insensitive) analysis of the output signal recorded during the #ight tests performed in the neighbourhood of the critical condition (#utter) may be desirable together with the capability to record the non-linear system signature. The time-scale decompositions (CWT) have given the opportunity to analyze pre-and post-critical transient behaviour of a non-linear aeroelastic system and, thus, upon considering the analytical tool given by the singular perturbation analysis, to identify its linear and non-linear features. Applications include either two non-linear coupled oscillators or a typical section in a supersonic #ow.
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