Solution of problem of plane flow of gas past body in presence of circulation; solution obtained by CHAPLYGIN linear equations, assuming that K is constant. English translation from Prikladnaya Matematika i Mekhanika v 2 n 1 1947 p 105-18.


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    Title :

    Subsonic gas flow past wing profile


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1950


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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