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contributor authorL. He
contributor authorJ. D. Denton
date accessioned2017-05-08T23:42:55Z
date available2017-05-08T23:42:55Z
date copyrightJanuary, 1993
date issued1993
identifier issn0889-504X
identifier otherJOTUEI-28627#94_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112852
description abstractAn efficient coupled approach between inviscid Euler and integral boundary layer solutions has been developed for quasi-3-D unsteady flows induced by vibrating blades. For unsteady laminar and turbulent boundary layers, steady correlations are adopted in a quasi-steady way to close the integral boundary layer model. This quasi-steady adoption of the correlations is assessed by numerical test results using a direct solution of the unsteady momentum integral equation. To conduct the coupling between the inviscid and viscous solutions for strongly interactive flows, the unsteady Euler and integral boundary layer equations are simultaneously time-marched using a multistep Runge–Kutta scheme, and the boundary layer displacement effect is accounted for by a first order transpiration model. This time-resolved coupling method converges at conditions with considerable boundary layer separation.
publisherThe American Society of Mechanical Engineers (ASME)
titleInviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 1—Description of the Method
typeJournal Paper
journal volume115
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929222
journal fristpage94
journal lastpage100
identifier eissn1528-8900
keywordsBlades
keywordsUnsteady flow
keywordsBoundary layers
keywordsMomentum
keywordsFlow (Dynamics)
keywordsSeparation (Technology)
keywordsBoundary layer turbulence
keywordsDisplacement
keywordsEquations
keywordsIntegral equations AND Transpiration
treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 001
contenttypeFulltext


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