Abstract A technique is suggested for calculating the helicopter spatial motion and the stress-strain state of a skid landing gear in the course of landing with regard for the second landing impact; geometric, material and design nonlinearity of undercarriage springs deformation is taken into account. The comparison between the analysis results and experimental data is presented.


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    Titel :

    Modeling of landing of a helicopter with skid undercarriage with regard for the second landing impact


    Beteiligte:
    Mikhailov, S. A. (Autor:in) / Korotkov, L. V. (Autor:in) / Alimov, S. A. (Autor:in) / Nedel’ko, D. V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2011-09-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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