Abstract The discretization of the boundary value problem for laminated composite shells is based on the finite difference approach using the regular mesh with the constant grid step and the difference operators of the second order of accuracy. The dynamic relaxation method is proposed for the solution of the nonlinear problem. The evolutionary equations of the dynamic relaxation are constructed, and the optimum parameters of the converging linear iterative process are estimated.


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    Titel :

    Nonlinear deforming of laminated composite shells of revolution under finite deflections and normal’s rotation angles


    Beteiligte:
    Dmitriev, V. G. (Autor:in) / Biryukov, V. I. (Autor:in) / Egorova, O. V. (Autor:in) / Zhavoronok, S. I. (Autor:in) / Rabinskii, L. N. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 60 , 2 ; 169-176


    Erscheinungsdatum :

    01.04.2017


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Nonlinear deforming of laminated composite shells of revolution under finite deflections and normal’s rotation angles

    Dmitriev, V. G. / Biryukov, V. I. / Egorova, O. V. et al. | Online Contents | 2017



    Calculation of finite axisymmetric deflections of thin short shells of revolution

    Grigolyuk, E. I. / Lopanitsyn, E. A. | British Library Online Contents | 1996