Derivation of basic theory and comparisons with axial machines; efficiency of centrifugal is lower than that of axial compressors; for given performance, centrifugal is much lighter than axial, and is preferable on grounds of simplicity and robustness; problem of fouling up of working surface is of much less importance in centrifugal than axial; disadvantage of centrifugal when used in aircraft, is large frontal diameter which gives rise to high drag. (See also - discussion n 284 Oct p 319)


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    Titel :

    Some notes on centrifugal compressors


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Thompson, L.N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1952


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Some Notes on Centrifugal Compressors

    Thompson, L.N. | Emerald Group Publishing | 1952


    Notes on Centrifugal Compressors

    Thompson | Emerald Group Publishing | 1952


    Centrifugal compressors

    Society of Automotive Engineers | TIBKAT | 1961



    Control of centrifugal compressors

    Moore, Ralph L. | TIBKAT | 1989