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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Heaslet, M.A. (author) / Lomax, H. (author)


    Publication date :

    1948


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English