Reinvestigation of theory with special reference to study of manner in which value of so-called critical Mach number for symmetrical Joukowski airfoil varies with angle of attack as well as with thickness ratio of airfoil. (In English.)


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    Title :

    On subsonic flow of compressible fluid past symmetrical Joukowski aerofoil


    Additional title:

    Tokyo Imperial Univ -- Aeronautical Research Inst -- Report


    Contributors:
    Tomotika, S. (author) / Umemoto, H. (author)


    Publication date :

    1941


    Size :

    91 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Compressible flow about symmetrical Joukowski profiles

    Kaplan, C. | Engineering Index Backfile | 1938


    Compressible flow about symmetrical joukowski profiles

    Kaplan, C. | Engineering Index Backfile | 1938


    Compressible flow about symmetrical joukowski profiles

    Kaplan, C. | Engineering Index Backfile | 1938


    A generalised type of Joukowski aerofoil

    Glauert, H. | TIBKAT | 1924