Performance of NACA Eight-Stage Axial-Flow Compressor Designed on Basis of Airfoil Theory. (Originally issued as Advance Confidential Report E4H18 Aug 1944)


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    Title :

    Performance of NACA eight-stage axial-flow compressor designed on basis of airfoil theory


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1943


    Size :

    35 pages


    Remarks:

    Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English