Perturbation field induced by line vortex in supersonic stream and downwash behind supersonic lifting surfaces are examined for purpose of establishing approximate methods for determining downwash behind supersonic wings; lifting line methods are presented for calculating supersonic downwash.


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    Title :

    Line vortex theory for calculation of supersonic downwash


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Mirels, H. (author) / Haefeli, R.C. (author)


    Publication date :

    1949


    Size :

    54 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Line-vortex theory for calculation of supersonic downwash

    Mirels, H. / Haefeli, R.C. | Engineering Index Backfile | 1950


    Line-vortex theory for calculation of supersonic downwash

    Mirels, Harold / Haefeli, Rudolph C. | TIBKAT | 1949


    Line-vortex theory for calculation of supersonic downwash

    Mirels, Harold / Haefeli, Rudolph C | NTRS | 1949


    Downwash behind wings at supersonic speeds

    Jacobs, W. | Engineering Index Backfile | 1955


    Note on evaluation of supersonic downwash integral

    Hunn, B.A. | Engineering Index Backfile | 1954