Aerodynamic influence of wings on tailplane loads; downwash induced in plane of symmetry of aircraft when wings have straight leading edges whose sweepback is such that they are subsonic in supersonic main stream; downwash due to delta wing at incidence, having simple triangular planform, case of swallow tail wings.


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    Title :

    Note on evaluation of supersonic downwash integral


    Additional title:

    Aeronautical Quarterly


    Contributors:
    Hunn, B.A. (author)

    Published in:

    Publication date :

    1954


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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