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contributor authorJ. P. Johnston
contributor authorS. A. Eide
date accessioned2017-05-08T23:00:56Z
date available2017-05-08T23:00:56Z
date copyrightSeptember, 1976
date issued1976
identifier issn0098-2202
identifier otherJFEGA4-26897#374_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88777
description abstractA method for calculation of turbulent boundary layers on curved, rotating surfaces is presented, and the applicability of the method to the prediction of attached flow over compressor rotor blades is indicated. Calculated results are compared to existing data sets. Additional sample calculations to study the effects of rotation are also presented. Correlations of these calculated results provide a simple method for estimation of the effects of rotation on skin friction, cf , and boundary-layer shape factor, H.
publisherThe American Society of Mechanical Engineers (ASME)
titleTurbulent Boundary Layers on Centrifugal Compressor Blades: Prediction of the Effects of Surface Curvature and Rotation
typeJournal Paper
journal volume98
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3448327
journal fristpage374
journal lastpage381
identifier eissn1528-901X
keywordsCompressors
keywordsRotation
keywordsBlades
keywordsBoundary layer turbulence
keywordsShapes
keywordsFlow (Dynamics)
keywordsSkin friction (Fluid dynamics)
keywordsBoundary layers AND Rotors
treeJournal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003
contenttypeFulltext


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