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  5. Mathematical model to estimate dry friction damper influence to aerodynamic aircraft control surfaces vibration amplitude in case of transonic flutter

Mathematical model to estimate dry friction damper influence to aerodynamic aircraft control surfaces vibration amplitude in case of transonic flutter

A. Safronov, A. Nedil’ko, V. Safrоnov
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A mathematical model to estimate dry friction damper influence to aerodynamic control surfaces vibration amplitude of supersonic and hypersonic aircraft in case of transonic flutter. Mathematical models could be using for estimation of another parameters influence to aerodynamic control surfaces vibration amplitude.
Keywords: mathematical model, aerodynamic control surface, the hinge moment, dry friction damper, transonic flutter