The General Rotorcraft Aeromechanical Stability Program (GRASP) was developed to analyze the steady-state and linearized dynamic behaviour of rotorcraft in hovering and axial flight conditions. Because of the nature of problems GRASP was created to solve, the geometrically nonlinear behaviour of beams is one area in which the program must perform well in order to be of any value. Numerical results obtained from GRASP are comupred to both static and dynamic experimental data obtained for a cantilever beam undergoing large displacements and rotations caused by deformation. The correlation is excellent in all cases.


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    Titel :

    Nonlinear analysis of a cantilever beam


    Weitere Titelangaben:

    Nichtlineare Analyse eines freitragenden Traegers


    Beteiligte:
    Hinnant, H.E. (Autor:in) / Hodges, D.H. (Autor:in)

    Erschienen in:

    AIAA Journal ; 26 , 12 ; 1521-1527


    Erscheinungsdatum :

    1988


    Format / Umfang :

    7 Seiten, 13 Bilder, 1 Tabelle, 13 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Nonlinear analysis of a cantilever beam

    HINNANT, HOWARD E. / NASA, Langley Research Center / Hampton, VA et al. | AIAA | 1988


    Nonlinear analysis of a cantilever beam

    Hinnant, Howard E. / Hodges, Dewey H. | NTRS | 1988


    Application of GRASP to nonlinear analysis of a cantilever beam

    HINNANT, HOWARD / HODGES, DEWEY | AIAA | 1987


    Application of GRASP to nonlinear analysis of a cantilever beam

    Hinnant, Howard E. / Hodges, Dewey H. | NTRS | 1987


    Cantilever beam linkage

    PUL GEORGE | Europäisches Patentamt | 2019

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