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 :

    01.01.1950


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Calculation of downwash behind supersonic wings with application to triangular plan forms

    Heaslet, M.A. / Lomax, H. | Engineering Index Backfile | 1948


    Calculation of downwash behind supersonic wings with application to triangular plan forms

    Lomax, H. / Sluder, L. / Heaslet, M.A. | Engineering Index Backfile | 1950




    Downwash behind wings at supersonic speeds

    Jacobs, W. | Engineering Index Backfile | 1955