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contributor authorR. C. Strawn
contributor authorS. J. Kline
date accessioned2017-05-08T23:15:51Z
date available2017-05-08T23:15:51Z
date copyrightMarch, 1983
date issued1983
identifier issn0098-2202
identifier otherJFEGA4-26993#28_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97292
description abstractAn inverse design method is presented which gives the user control over stall margin, or distance from detachment, along the walls of planar and axisymmetric diffusers. It is proposed that optimum diffuser designs have continuous incipient detachment along their wall boundary layers. This hypothesis is supported by experimental and computational results plus physical arguments concerning the detachment process. Several computed optimum planar diffuser shapes are presented and discussed. For short diffusers with healthy inlet boundary layers, these optimum shaped wall units can have significantly higher pressure recovery than their straight-wall counterparts (up to 40 percent higher Cp in certain favorable cases). In most cases, however, the gains from wall contouring are small when compared to optimum straight-wall designs. This paper differs from earlier discussion in two ways: (i) it employs an improved physical model and correlation of detachment, and (ii) it uses improved boundary layer procedures based on (i).
publisherThe American Society of Mechanical Engineers (ASME)
titleA Stall Margin Design Method for Planar and Axisymmetric Diffusers
typeJournal Paper
journal volume105
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3240936
journal fristpage28
journal lastpage33
identifier eissn1528-901X
keywordsDiffusers
keywordsDesign methodology
keywordsBoundary layers
keywordsShapes AND Pressure
treeJournal of Fluids Engineering:;1983:;volume( 105 ):;issue: 001
contenttypeFulltext


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