This final paper of the series deals with the application of the structural and aerodynamic matrices to determine the final steady state loading on the wing, with a view to the requirements of the stress analyst. It is also shown how the stability derivatives of the elastic wing may be obtained, if a system of unit loads is employed in the calculations. Finally the occurrence of wing divergence and control surface reversal speeds are discussed in the light of the proposed methods.


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    Titel :

    Aeroelastic Problems of Low Aspect Ratio Wings


    Untertitel :

    Part V. Application of the Structural and Aeroelastic Matrices to the Solution of Steady State Aeroelastic Problems


    Beteiligte:
    Farbridge, J.E.F. (Autor:in) / Woodward, F.A. (Autor:in) / Thomann, G.E.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.06.1956


    Format / Umfang :

    3 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Aeroelastic Problems of Low Aspect Ratio Wings

    Leyds, J. | Emerald Group Publishing | 1956


    Aeroelastic Problems of Low Aspect Ratio Wings

    Leyds, J. | Emerald Group Publishing | 1956


    Aeroelastic Problems of Low Aspect Ratio Wings

    Woodward, F.A. | Emerald Group Publishing | 1956


    Aeroelastic Problems of Low Aspect Ratio Wings

    Thomann, G.E.A. | Emerald Group Publishing | 1956


    Nonlinear aeroelastic scaling of high aspect-ratio wings

    Spada, Christian | Online Contents | 2017