Summary
We consider general theoretical issues of the aeroelastic fluid-structure-interaction. In particular we have chosen an elastic panel in transonic flow as our model problem for computational experiments. First we consider the question of well-posedness of the equation system, giving a uniqueness result. Numerical simulations address the choice of the structural model and the choice of the time-marching-scheme that couples the equations of fluid and structure.
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Massjung, R., Hurka, J., Dahmen, W., Ballmann, J. (2003). On Well-Posedness and Modelling for Nonlinear Aeroelasticity. In: Ballmann, J. (eds) Flow Modulation and Fluid—Structure Interaction at Airplane Wings. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 84. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-44866-2_9
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DOI: https://doi.org/10.1007/978-3-540-44866-2_9
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