2006
DOI: 10.1007/s00033-006-0080-7
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Dynamics of a thermoelastic von Kármán plate in a subsonic gas flow

Abstract: We discuss the problem of non-linear oscillations of a clamped thermoelastic plate in a subsonic gas flow. The dynamics of the plate is described by von Kármán system in the presence of thermal effects. No mechanical damping is assumed. To describe the influence of the gas flow we apply the linearized theory of potential flows. Our main result states that each weak solution of the problem considered tends to the set of the stationary points of the problem.A similar problem was considered in [27], but with rota… Show more

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Cited by 26 publications
(73 citation statements)
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References 13 publications
(42 reference statements)
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“…Well-posedness results in the past literature deal mainly with the dynamics possessing some regularizing effects. This has been accomplished by either accounting for non-negligible rotational inertia [10,12,22] and strong damping of the form −α∆u t , or by incorporating helpful thermal effects into the structural model [57,58]. In the cases listed above, the natural structure of the dynamics dictate that the plate velocity has the property u t ∈ H 1 (Ω), which provides the needed regularity for the applicability of many standard tools in nonlinear analysis.…”
Section: Well-posedness Of Nonlinear Panel Modelmentioning
confidence: 99%
“…Well-posedness results in the past literature deal mainly with the dynamics possessing some regularizing effects. This has been accomplished by either accounting for non-negligible rotational inertia [10,12,22] and strong damping of the form −α∆u t , or by incorporating helpful thermal effects into the structural model [57,58]. In the cases listed above, the natural structure of the dynamics dictate that the plate velocity has the property u t ∈ H 1 (Ω), which provides the needed regularity for the applicability of many standard tools in nonlinear analysis.…”
Section: Well-posedness Of Nonlinear Panel Modelmentioning
confidence: 99%
“…. This is given as Lemma 10 in [39, p. 472] (where it is proved) and is utilized in a critical way in [40] as well.…”
Section: )mentioning
confidence: 99%
“…Our result implies that flutter (a periodic or chaotic end behavior) can be eliminated (in subsonic flows) with sufficient frictional damping in the structure. While such a result has been proved in the past for regularized plate models (with rotational inertia terms or thermal considerations [14,32,39,40]), this is the first treatment which does not incorporate smoothing effects for the structure.…”
mentioning
confidence: 91%
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