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)
Some shrouding and tip clearance effects in axial flow compressors
North East Coast Instn Engrs Shipbldrs -- Trans
1958
50 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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