Abstract The classification of methods for carrier-based aircraft wing folding is presented. We determined the factors influencing the folding axis position and the mass increase of the wing being folded. We also suggested a technique of deriving the folding wing mass formula by an example of the wing rotation around the axis, which is parallel to the aircraft plane of symmetry.


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    Titel :

    Development of the weight formula for a folding wing


    Beteiligte:
    Yarygina, M. V. (Autor:in) / Popov, Yu. I. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.04.2012


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Development of the weight formula for a folding wing

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