The study extends Prandtl's lifting-line theory to planar wings involving swept and curved centerlines. Attention is focused on distinct features of such a theory, with special emphasis on an oblique wing in a steady incompressible potential flow. The analysis presented is compared with exact solutions derived from an inverse method and with results from a panel method.


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    Title :

    Lifting-line theory of oblique wings


    Contributors:

    Published in:

    Publication date :

    1978-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Lifting-Line Theory of Oblique Wings

    H. K. Cheng | AIAA | 1978


    Lifting-line theory of oblique wings in transonic flows

    Cheng, H. K. / Meng, S. Y. | NTRS | 1979


    Lifting-Line Theory of Oblique Wings in Transonic Flows

    H. K. Cheng / S. Y. Meng | AIAA | 1979


    Lifting-Line Theory of Oblique Wings in Transonic Flows

    H. K. Cheng / S. Y. Meng | NTIS | 1978


    Lifting-Line Theory for Arbitrarily Shaped Wings

    M. L. Rasmussen / D. E. Smith | AIAA | 1999