Abstract
We consider a subsonic flow-structure interaction describing the flow of gas above a flexible plate. A perturbed wave equation describes the flow, and a second-order nonlinear plate equation describes the plate's displacement. We consider the model that accounts for rotational inertia in the plate, parametrized by 0. It is known that the presence of > 0 has strong effect on regularity properties of the plate, which then allows one to establish well-posedness of finite energy solutions for the entire structure. In this paper, it is shown that semigroup well-posedness of the model is not only preserved for all 0 but that the corresponding nonlinear semigroups S(t) converge to S-0(t) when 0. The above result holds also in the presence of nonlinear boundary damping. In addition, we provide a discussion of the regularity of strong solutions. Copyright (c) 2011 John Wiley & Sons, Ltd.
| Original language | English |
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| Journal | Mathematical Methods in the Applied Sciences |
| State | Published - 2013 |