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contributor authorD. E. Paxson
contributor authorR. E. Mayle
date accessioned2017-05-08T23:36:56Z
date available2017-05-08T23:36:56Z
date copyrightJuly, 1991
date issued1991
identifier issn0889-504X
identifier otherJOTUEI-28613#419_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109383
description abstractAn investigation was conducted to study the unsteady effects of a moving wake as it passes over a laminar boundary layer in a stagnation region. Arguments are presented showing that in this region, the wake-induced unsteadiness may be treated, for the most part, as an inviscid, unsteady free stream, which impresses itself on the boundary layer flow. As a result, the boundary layer equations remain valid and, for relatively small oscillations, a solution to the equations may be obtained using standard perturbation techniques. A related experiment is then described and the results are examined in light of this analytical approach.
publisherThe American Society of Mechanical Engineers (ASME)
titleLaminar Boundary Layer Interaction With an Unsteady Passing Wake
typeJournal Paper
journal volume113
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927891
journal fristpage419
journal lastpage427
identifier eissn1528-8900
keywordsWakes
keywordsBoundary layers
keywordsEquations
keywordsOscillations AND Flow (Dynamics)
treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
contenttypeFulltext


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