A dynamical model is presented to analyse the stability of motion of the two-wheeled ‘Fokker F.28-like’ landing gear including tyres. The model is equally applicable to similar landing gears. The influence of the introduction of a specially designed torsional damper on the dynamical behaviour of the landing gear-tyre combination is investigated. Results of the stability calculations are supported by test results.


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    Titel :

    An Analysis of a Civil Aircraft Main Gear Shimmy Failure


    Beteiligte:
    VAN DER VALK, R. (Autor:in) / PACEJKA, H.B. (Autor:in)

    Erschienen in:

    Vehicle System Dynamics ; 22 , 2 ; 97-121


    Erscheinungsdatum :

    01.01.1993




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt



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