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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Quadrilateral ‘Shear’ Panel


    Subtitle :

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


    Contributors:

    Published in:

    Publication date :

    1951-05-01


    Size :

    11 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    QUADRILATERAL CONNECTING ROD STRUCTURE

    YANG XIANG / HE QINGHUA / ZHU JIANXIN et al. | European Patent Office | 2021

    Free access

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

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


    MOTORCYCLE WITH QUADRILATERAL REAR SUSPENSION

    RAFFAELLI ANDREA | European Patent Office | 2023

    Free access

    Optimal Hierarchies for Quadrilateral Surfaces

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