Approximate linearized solution is obtained from source distribution about cylinder and is accurate for limiting case of ring airfoils having small chord-radius ratios.


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    Titel :

    Theoretical wave drag and lift of thin supersonic ring airfoils


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Mirels, H. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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