Results for cascades of airfoils as corresponds to case of impeller of axial propeller pump and propeller fan; lift and pressure drag coefficients on center section of 6, 7, and 9-section cascades are compared with results from tests of single airfoil. English translation from Soc Mech Engrs, Japan -- Trans v 3 n 12 Nov 1937.


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    Title :

    Tests of cascades of airfoils for retarded flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1947


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Tests of Cascades of Airfoils for Retarded Flow

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    Shimoyama, Yoshinori | TIBKAT | 1947


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    KORAKIANITIS, THEODOSIOS P. | AIAA | 1989