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contributor authorO. E. Baljé
date accessioned2017-05-09T00:35:56Z
date available2017-05-09T00:35:56Z
date copyrightJuly, 1970
date issued1970
identifier issn1528-8919
identifier otherJETPEZ-26687#275_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142233
description abstractRelations are derived for the boundary layer momentum thickness growth in channels with adverse pressure gradients and for the maximum allowable momentum thickness to avoid flow separation. These data are obtained by integrating the Truckenbrodt equation stepwise and by extending the Gruschwitz-Schmidbauer separation criterion. Fair agreement between calculated data and test information is demonstrated.
publisherThe American Society of Mechanical Engineers (ASME)
titleLoss and Flow Path Studies on Centrifugal Compressors—Part I
typeJournal Paper
journal volume92
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445352
journal fristpage275
journal lastpage286
identifier eissn0742-4795
keywordsMomentum
keywordsFlow (Dynamics)
keywordsSeparation (Technology)
keywordsChannels (Hydraulic engineering)
keywordsCompressors
keywordsBoundary layers
keywordsEquations
keywordsFlow separation
keywordsPressure gradient AND Thickness
treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
contenttypeFulltext


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