Method developed consistent with assumptions of small perturbation theory, which provides means of determining downwash behind wing in supersonic flow for known load distribution; analysis based upon use of supersonic doublets distributed over plan form and wake of wing in manner determined from wing loading.


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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Heaslet, M.A. (Autor:in) / Lomax, H. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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