In supersonic flow about isolated bodies, large energy losses usually occur due to wave systems which extend far from bodies; supersonic flow entering cascade is considered and possibility of entirely eliminating this extended wave system is demonstrated; thus, there is no reason for supersonic compressors to be necessarily inefficient; because of encouraging results, experimental single stage supersonic compressor has been constructed and tested in Freon-12. (15¢)


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    Titel :

    Supersonic axial-flow compressor


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Kantrowitz, A. (Autor:in)


    Erscheinungsdatum :

    1950


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic Axial-Flow Compressor

    A. Kantrowitz | NTIS | 1946


    The Supersonic Axial-Flow Compressor

    Kantrowitz, Arthur | NTRS | 1950


    Investigation of an Experimental Supersonic Axial-Flow Compressor

    J. R. Erwin / L. C. Wright / A. Kantrowitz | NTIS | 1947


    Investigation of an Experimental Supersonic Axial-Flow Compressor

    Erwin, John R. / Wright, Linwood C. / Kantrowitz, Arthur | NTRS | 1947


    Investigation of an Experimental Supersonic Axial-Flow Compressor

    J. R. Erwin / L. C. Wright / A. Kantrowitz | NTIS | 1947