1989
DOI: 10.2514/3.10084
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Localization of vibrations in large space reflectors

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Cited by 53 publications
(12 citation statements)
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“…the one presented in Fig. 1 may be understood as a minimal model of different aerospace structures, such as space reflectors [3], disk antennas [28] and bladeddisks of aero-engines [6,7]. In the case of bladed-disk vibrations, the model presented in Fig.…”
Section: The Model and Solution Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…the one presented in Fig. 1 may be understood as a minimal model of different aerospace structures, such as space reflectors [3], disk antennas [28] and bladeddisks of aero-engines [6,7]. In the case of bladed-disk vibrations, the model presented in Fig.…”
Section: The Model and Solution Methodsmentioning
confidence: 99%
“…Localisation of vibrations has received considerable attention from the structural dynamics engineering community over the last three decades (see e. g. papers [1,2,3,4,5,6,7,8] and references therein). In a linear framework, localisa-tion may arise due to imperfections in the manufacturing process that result in a slightly disordered and inhomogeneous system.…”
Section: Introductionmentioning
confidence: 99%
“…qualitative changes in system dynamics (see e.g. [19][20][21][22][23][24][25][26][27][28]). Nonlinear localization has been shown to appear not only in conservative systems [19] but also in friction-excited chains of weakly coupled oscillators [20,21], where the authors showed that the localization phenomenon is strongly related to the bistable behaviour of the single oscillator in the chain.…”
Section: Introductionmentioning
confidence: 99%
“…(39), the forced response in physical coordinates follows from Eq. (57) and is given by q ss ðtÞ ¼ e nþ1 u ss nþ1 ðtÞ (77) where e nþ1 is the ðn þ 1Þth column of the Fourier matrix and u ss nþ1 ðtÞ is given by Eq. (76).…”
Section: Forced Response Of a General Cyclic System Undermentioning
confidence: 99%