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contributor authorI. M. Khalil
contributor authorW. Tabakoff
contributor authorA. Hamed
date accessioned2017-05-08T23:00:56Z
date available2017-05-08T23:00:56Z
date copyrightSeptember, 1976
date issued1976
identifier issn0098-2202
identifier otherJFEGA4-26897#364_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88776
description abstractA study was conducted to determine experimentally and theoretically the losses in radial inflow turbine nozzles. Extensive experimental data were obtained to investigate the flow behavior in a full-scale radial turbine stator annulus. A theoretical model to predict the losses in both the vaned and vaneless regions of the nozzle was developed. In this analysis, the interaction effects between the stator and the rotor are not considered. It was found that the losses incurred due to the end wall boundary layers can be significant, especially if they are characterized by a strong crossflow. The losses estimated using the analytical study are compared with the experimentally determined values.
publisherThe American Society of Mechanical Engineers (ASME)
titleLosses in Radial Inflow Turbines
typeJournal Paper
journal volume98
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3448323
journal fristpage364
journal lastpage371
identifier eissn1528-901X
keywordsTurbines
keywordsInflow
keywordsStators
keywordsNozzles
keywordsRotors
keywordsFlow (Dynamics)
keywordsBoundary layers AND Annulus
treeJournal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003
contenttypeFulltext


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