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    Titel :

    Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory


    Beteiligte:
    King, J Austin (Autor:in)

    Erscheinungsdatum :

    01.08.1944


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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

    Sinnette, Jr., J.T. / Schey, O.W. / King, J.A. | Engineering Index Backfile | 1943


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

    Sinnette, Jr., J.T. / Schey, O.W. / King, J.A. | Engineering Index Backfile | 1943


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

    Sinnette, John T. / Schey, Oscar W. / King, J. Austin | TIBKAT | 1944


    Performance of NACA eight-stage axial-flow compressor at simulated altitudes

    King, J.A. / Regan, O.W. | Engineering Index Backfile | 1944