Drag of straight and swept wings between parallel walls at high subsonic Mach numbers as well as at Mach numbers in transonic and supersonic ranges; object is to provide estimation of wall interferences and thus of magnitude of effective sweep angle of wings between parallel walls in transonic range.


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    Title :

    Transonic flow past swept and unswept wings between parallel walls


    Additional title:

    Stockholm. Flygtekniska Forsoksanstalten (Aeronautical Research Inst, Sweden) -- Report


    Contributors:
    Jacobs, W. (author)


    Publication date :

    1954


    Size :

    34 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Transonic flow past swept wings

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    Improved calculation of transonic potential flow past swept wings

    WANG, LIXIA / CAUGHEY, DAVID A. | AIAA | 1992


    Buffet Alleviation on Swept and Unswept Wings at High Incidence

    G. A. Flynn / J. F. Morrison / D. G. Mabey | AIAA | 2001