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    Title :

    Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers IV : performance of tapered-tip rotor configuration with reset blade angles


    Contributors:

    Publication date :

    1957-02-28


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English