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Investigation of landing gear wheel shimmy taking into account damper frequency characteristics
Authors:V. S. Metrikin  M. A. Peisel’
Affiliation:(1) Research Institute of Applied Mathematics and Cybernetics, N.I. Lobachevskii State University, Nizhni Novgorod, Russia;(2) OAO Gidromash, Nizhni Novgorod, Russia
Abstract:A mathematical model and a technique for calculating the rolling motion stability of the damper-equipped landing gear wheel are presented; the dependence of dynamic damper rigidity on frequency found experimentally is used in the investigation. The results of calculating the shimmy boundaries with and without regard for the dependence indicated are given.
Keywords:landing gear  shimmy  stability  damper  amplitude  frequency  dynamic rigidity  wheel rolling
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