Series of tests relative to economics of blade manufacture, at National Gas Turbine Establishment; it is concluded shrouding should be avoided if possible; if used, clearance should be at smallest practicable value; use of very fine radial tip clearances may also result in loss of performance. (See also - discussion n 7 May/June p D69-76; Int Shipbldg Progress v 5 n 42 Feb 1958 p 78-101)


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    Titel :

    Some shrouding and tip clearance effects in axial flow compressors


    Weitere Titelangaben:

    North East Coast Instn Engrs Shipbldrs -- Trans


    Beteiligte:
    Jefferson, J.L. (Autor:in) / Turner, R.C. (Autor:in)


    Erscheinungsdatum :

    1958


    Format / Umfang :

    50 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Some shrouding and tip clearance effects in axial flow compressors1

    Jefferson, J.L. / Turner, R.C. | IOS Press | 1958



    The Structure of Tip Clearance Flow in Axial Flow Compressors

    Lakshminarayana, B. | Online Contents | 1995


    Control of tip clearance flows in axial compressors

    Bae, J. / Tan, C. / Breuer, K. | AIAA | 2000