Abstract
In this chapter we return to the full nonlinear aeroelastic problem as stated in Chap. 3, with the structure models both linear and nonlinear, described in Chap. 2 and the isentropic aerodynamics as treated in Chap. 3 with the flow tangency and the Kutta–Joukowsky boundary conditions. Recall that we use continuum models without immediately approximating them by finite-dimensional models as in all the current aeroelastic literature.
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Balakrishnan, A.V. (2012). Nonlinear Aeroelasticity Theory in 2D Aerodynamics: Flutter Instability as an LCO. In: Aeroelasticity. Springer, New York, NY. https://doi.org/10.1007/978-1-4614-3609-6_6
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DOI: https://doi.org/10.1007/978-1-4614-3609-6_6
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