IN Part I the motion of an aircraft, designated by the position-tensor X, was considered relative to a fixed reference frame E. Now in our analysis of the motion of a wing, designated by the position-tensor U, the relevant reference frame is X, though X is still free to move relative to E. The hinge on which the wing moves in the aircraft is denoted by the unit vector h, and for any specified hinge-axis the components of h with respect to both U and X will have fixed values. The basic notation, following the principles adopted in Part I, Section (2), is therefore


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    Titel :

    Tensor Analysis of Finite Rotations


    Untertitel :

    Applications to Aircraft Manoeuvres, Variable Sweep Wings, Retractable Undercarriages


    Beteiligte:
    Bateman, E.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1958-06-01


    Format / Umfang :

    3 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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