Abstract A model of the main support of the aircraft landing gear is presented and its dynamics is studied using the equations for the distributed motion of a wheel equipped with a brake. Stability of the support wheel rolling motion is analyzed and the brake parameter values which may cause stability loss are found. The results of numerical experiments are presented.
Calculation of flight vehicle main support wheel vibrations taking into account brake forces
Russian Aeronautics (Iz VUZ) ; 55 , 2 ; 144-150
2012-04-01
7 pages
Article (Journal)
Electronic Resource
English
Calculation of flight vehicle main support wheel vibrations taking into account brake forces
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