Nonlinear Aeroelasticity Theory in 2D Aerodynamics: Flutter Instability as an LCO

A V Balakrishnan
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A V Balakrishnan: University of California, Department of Electrical Engineering Department of Mathematics

Chapter Chapter 6 in Aeroelasticity, 2012, pp 269-326 from Springer

Abstract: 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.

Keywords: Hopf Bifurcation; Nonlinear Case; Pressure Jump; Limit Cycle Oscillation; Time Domain Operator (search for similar items in EconPapers)
Date: 2012
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DOI: 10.1007/978-1-4614-3609-6_6

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