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.
Investigation of landing gear wheel shimmy taking into account damper frequency characteristics
Russian Aeronautics (Iz VUZ) ; 52 , 2 ; 240-244
2009-06-01
5 pages
Article (Journal)
Electronic Resource
English
Investigation of landing gear wheel shimmy taking into account damper frequency characteristics
Online Contents | 2009
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