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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    Title :

    Theoretical wave drag and lift of thin supersonic ring airfoils


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Mirels, H. (author)


    Publication date :

    1948


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :