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contributor authorR. L. Stoy
contributor authorY. Ben-Haim
date accessioned2017-05-09T01:36:31Z
date available2017-05-09T01:36:31Z
date copyrightDecember, 1973
date issued1973
identifier issn0098-2202
identifier otherJFEGA4-26851#551_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163861
description abstractAn experimental and analytical study of the deflection and impingement of turbulent jets in a confined crossflow, a geometry which occurs in gas turbine blade impingement cooling schemes, is presented. The range of jet and crossflow Reynolds numbers investigated is directly applicable to turbine blade configuratons. A simple one-dimensional analysis using the basic conservation equations is developed to predict jet trajectory, average jet properties, and impingement point for spatially variable crossflow velocity profiles. The simplicity of the one-dimensional analysis makes it more suited to design calculations than two-dimensional jet analyses. Other crossflow velocity profiles are studied and jet development is successfully predicted by the analysis for all cases.
publisherThe American Society of Mechanical Engineers (ASME)
titleTurbulent Jets in a Confined Crossflow
typeJournal Paper
journal volume95
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3447069
journal fristpage551
journal lastpage556
identifier eissn1528-901X
keywordsJets
keywordsTurbulence
keywordsReynolds number
keywordsTurbine blades
keywordsTrajectories (Physics)
keywordsDesign
keywordsGas turbines
keywordsImpingement cooling
keywordsBlades
keywordsDeflection
keywordsEquations AND Geometry
treeJournal of Fluids Engineering:;1973:;volume( 095 ):;issue: 004
contenttypeFulltext


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