Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental Investigation of an Axial Flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers I : Over-all Performance of Stage with Transonic Rotor and Subsonic Stators up to Rotor Relative Inlet Mach Number of 1.1


    Contributors:

    Publication date :

    1952-03-10


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English