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contributor authorJ. H. Horlock
contributor authorJ. F. Louis
contributor authorP. M. E. Percival
contributor authorB. Lakshminarayana
date accessioned2017-05-08T23:43:31Z
date available2017-05-08T23:43:31Z
date copyrightSeptember, 1966
date issued1966
identifier issn0098-2202
identifier otherJFEGA4-27283#637_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113201
description abstractThe “wall stall” in compressor cascades has been observed by many research workers. There is a region of high loss in the corner bounded by the end wall and the suction surface of a blade. It is the separation of the flow in this region which is largely responsible for the increase in the axial velocity across the midspan section of the blades when there is no end-wall suction. It is important to differentiate between this wall stall and the two-dimensional stall of the blading. The work on wall stall described in the paper was carried out at the University of Cambridge and the University of Liverpool in the period 1955-1962.
publisherThe American Society of Mechanical Engineers (ASME)
titleWall Stall in Compressor Cascades
typeJournal Paper
journal volume88
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3645925
journal fristpage637
journal lastpage648
identifier eissn1528-901X
keywordsCompressors
keywordsSuction
keywordsBlades
keywordsCorners (Structural elements)
keywordsFlow (Dynamics) AND Separation (Technology)
treeJournal of Fluids Engineering:;1966:;volume( 088 ):;issue: 003
contenttypeFulltext


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