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.


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    Titel :

    Calculation of flight vehicle main support wheel vibrations taking into account brake forces


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2012-04-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch







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