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    Title :

    Effect of squealer tip geometry on rotor blade aerodynamic performance


    Contributors:

    Published in:

    Hang kong xue bao ; 34 , 2 ; 218-226


    Publication date :

    2013



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Chinese



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik






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