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contributor authorM. V. Finnis
contributor authorA. Brown
date accessioned2017-05-08T23:52:03Z
date available2017-05-08T23:52:03Z
date copyrightJanuary, 1996
date issued1996
identifier issn0889-504X
identifier otherJOTUEI-28648#162_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117905
description abstractMeasurements are presented of the streamwise velocity variation within a laminar boundary layer on a concave surface of 4 m radius of curvature for which the free-stream velocity gradient factor (ν/U0 2 )dU0 /dx was approximately 1 × 10−6 . The stream velocity variation was consistent with the presence of counterrotating vortices resulting from the Görtler instability. The vortices exhibited exponential growth over the streamwise extent of the measurements to a disturbance amplitude of approximately 13 percent of the local free-stream velocity. The vortex growth rates were found to be less than those for a zero velocity gradient factor, indicating that a favorable pressure gradient stabilizes the flow with respect to the Görtler instability. Boundary layer profiles at local upwash and downwash positions are compared with the linear theory for which the mean flow was modeled using the Pohlhausen approximation to the solution of the boundary layer equations. The agreement between the measured and predicted profiles indicates that the linear stability theory can provide a fair approximation to the small amplitude growth of the Görtler instability.
publisherThe American Society of Mechanical Engineers (ASME)
titleDarryl E. Metzger Memorial Session Paper: The Streamwise Development of Görtler Vortices in a Favorable Pressure Gradient
typeJournal Paper
journal volume118
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2836597
journal fristpage162
journal lastpage171
identifier eissn1528-8900
keywordsVortices
keywordsPressure gradient
keywordsBoundary layers
keywordsFlow (Dynamics)
keywordsMeasurement
keywordsGradients
keywordsApproximation
keywordsEquations AND Stability
treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 001
contenttypeFulltext


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