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    Title :

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


    Contributors:

    Published in:

    Publication date :

    1944


    Size :

    7 S., [10] Bl


    Remarks:

    Ill., graph. Darst
    Originally issued December 1944 as Advance confidential report E4L21
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik




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

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


    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