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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    Title :

    Aeroelastic Problems of Low Aspect Ratio Wings


    Subtitle :

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


    Contributors:

    Published in:

    Publication date :

    1956-06-01


    Size :

    3 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    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

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    Aeroelastic Problems of Low Aspect Ratio Wings

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