Dynamic distortion of supersonic wind tunnel for turbojet engines


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental investigation of dynamic distortion in a Mach 2.50 inlet with 60 percent internal contraction and its effect on turbojet stall margin


    Contributors:

    Publication date :

    1969-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English