In connection with tests of airplane cooling systems need was felt for information on axial fan design inasmuch as indications are that such fans will be used in airplane cooling systems in immediate future; fan tested comprised single 24-blade rotor having diam of 21 in. and solidity of 1.33; fan was tested for volume, pressure, and efficiency over range of delivery pressure and volumes for wide range of contravane and blade angle settings.


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    Title :

    Test of single-stage axial-flow fan


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1941


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :