Use of this analytical parameter, it is shown, highlights the distinction between cases which are dominated by trailing-edge separation, and those for which separation at the shock foot is dominant. Use of the analytical parameter and the distinction noted above greatly improves the correlation of separation data and the extrapolation of wind tunnel data to flight conditions.


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    Titel :

    New considerations on scale extrapolation of wing pressure distributions affected by transonic shock-induced separations


    Beteiligte:
    Kahn, M. M. S. (Autor:in) / Cahill, J. F. (Autor:in)

    Erscheinungsdatum :

    01.03.1983


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch