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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    Titel :

    Transonic flow past swept and unswept wings between parallel walls


    Weitere Titelangaben:

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


    Beteiligte:
    Jacobs, W. (Autor:in)


    Erscheinungsdatum :

    1954


    Format / Umfang :

    34 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Transonic flow past swept wings

    Caughey, D. A. / Jameson, A. | NTRS | 1980


    Comparison of advanced turboprop installation on swept and unswept supercritical wings at transonic speeds

    Carlson, J. R. / Pendergraft, O. C., Jr. / Bartlett, G. R. | NTRS | 1985



    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