1. Science
  2. Publications
  3. Scientific Works of Kharkiv National Air Force University
  4. 2(51)'2017
  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
Annotations languages:

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
Reference:
Safronov, O.V. (2017), "Matematychni modeli otsinky vplyvu dempferiv sukhoho tertia na riven kolyvan aerodynamichnykh poverkhon keruvannia litakiv pry vynyknenni transzvukovoho flateru" [Mathematical model to estimate dry friction damper influence to aerodynamic aircraft control surfaces vibration amplitude in case of transonic flutter], Scientific Works of Kharkiv National Air Force University, Vol. 2(51), pp. 76-80.