Potential increases in ideal stage pressure ratio theoretically possible in axial compressors; paper shows various configurations of flow diagram, for four individual cases, which result in considerable increases in ideal stage pressure ratio; considerations limited to ideal adiabatic flow through curved lattice types of blading.


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    Titel :

    High-speed flow through cambered rotating grids


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1948


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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