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    Title :

    Experimental Investigation of an Axial-flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers III : Blade-row Performance of Stage with Transonic Rotor and Subsonic Stator at Corrected Tip Speeds of 800 and 1000 Feet Per Secon


    Contributors:

    Publication date :

    1953-09-18


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English