Among the problems introduced by swept wings is that of the non-rectangular panel in equilibrium under loading applied tangentially along its edges. The present article examines the state of stress in a general uniform quadrilateral panel and, for the benefit of stiffness calculations, the strain energy stored in it. Stable conditions are assumed. The problem of replacing such a panel by ‘diamond’ bracing is also treated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Quadrilateral ‘Shear’ Panel


    Untertitel :

    The Peculiar Stressing Problems Arising in the Structure of the Non-Rectangular Swept Wing


    Beteiligte:
    Garvey, S.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.05.1951


    Format / Umfang :

    11 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Quadrilateral element panel method : QUADPAN ; user's manual ver. 3.2

    Youngren, Harold H. / Bouchard, Eugene E. / Coopersmith, Robert M. | TIBKAT | 1984


    Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory

    Alanbay, Berkan / Kapania, Rakesh K. / Batra, Romesh C. | AIAA | 2020


    QUADRILATERAL CONNECTING ROD STRUCTURE

    YANG XIANG / HE QINGHUA / ZHU JIANXIN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Optimal Hierarchies for Quadrilateral Surfaces

    Chung, K. L. / Yan, W. M. / Wu, J. G. | British Library Online Contents | 2002