The results of Murman and Krupp (1971) are used to develop a procedure for computing a transonic flow about a finite lifting wing. A small disturbance equation describing the velocity potential of three-dimensional wings is solved in the process. The procedure is applied to a wing with a symmetric biconvex airfoil section in a zero-incidence subsonic flow, to a supersonic rectangular lifting wing with a sharp leading edge and to a subcritical nonlifting rectangular wing with a blunt leading edge.


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    Titel :

    Computation of transonic flow about finite lifting wings.


    Beteiligte:
    Newman, P. A. (Autor:in) / Klunker, E. B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.07.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Computation of Transonic Flow about Finite Lifting Wings

    P.A. NEWMAN AND E.B. KLUNKER | AIAA | 1972


    Transonic flow past lifting wings.

    NORSTRUD, H. | AIAA | 1973



    Computation of viscous transonic flow about a lifting airfoil

    WALITT, L. / KING, L. / LIU, C. | AIAA | 1977