The flowfield in the plane of symmetry of a thin lifting delta wing with supersonic leading edges is examined for wings with apex angles that are comparable to the Mach angle, as well as for the limiting case of a straight leading edge. For these two cases, a simplified treatment of the interaction between the plane expansion wave emanating from the trailing edge and the three-dimensional bow shock is presented. In the region unaffected by the wing tips, the shock decays inversely with distance from the wing.


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    Titel :

    Flowfield in the plane of symmetry below a delta wing


    Beteiligte:
    Cramer, M. S. (Autor:in) / George, A. R. (Autor:in) / Seebass, A. R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Flowfield in the plane of symmetry below a delta wing

    CRAMER, M. S. / GEORGE, A. R. / SEEBASS, A. R. | AIAA | 1976


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