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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    Title :

    Some shrouding and tip clearance effects in axial flow compressors


    Additional title:

    North East Coast Instn Engrs Shipbldrs -- Trans


    Contributors:


    Publication date :

    1958


    Size :

    50 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Some shrouding and tip clearance effects in axial flow compressors1

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