A method is developed consistent with the assumptions of small perturbation theory which provides a means of determining the downwash behind a wing in supersonic flow for a known load distribution. The analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading. The equivalence in subsonic and supersonic flow of the downwash at infinity corresponding to a given load distribution is proved.


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    Titel :

    The calculation of downwash behind supersonic wings with an application to triangular plan forms


    Beteiligte:
    Lomax, Harvard (Autor:in) / Sluder, Loma (Autor:in) / Heaslet, Max A (Autor:in)

    Erscheinungsdatum :

    1950-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch