Aeroelastic modeling and stability analysis: A robust approach to the flutter problem

Summary In this paper, a general approach to address modeling of aeroelastic systems, with the final goal to apply μ analysis, is discussed. The chosen test bed is the typical section with unsteady aerodynamic loads, which enables basic modeling features to be captured and so extend the gained knowl...

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Veröffentlicht in:	International journal of robust and nonlinear control 2018-01, Vol.28 (1), p.342-364
Hauptverfasser:	Iannelli, Andrea, Marcos, Andrés, Lowenberg, Mark
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic loads Aerodynamics Aeroelastic stability Aeroelasticity Flutter Formulations LFT modeling Modelling robust analysis Stability analysis Transformations uncertain systems
Online-Zugang:	Volltext
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