Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers II : stage and blade-element performance


    Contributors:

    Publication date :

    1955-01-10


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English