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contributor authorJ. P. Gostelow
contributor authorN. Melwani
contributor authorG. J. Walker
date accessioned2017-05-08T23:51:50Z
date available2017-05-08T23:51:50Z
date copyrightOctober, 1996
date issued1996
identifier issn0889-504X
identifier otherJOTUEI-28655#737_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117803
description abstractA pressure distribution representative of a controlled diffusion compressor blade suction surface is imposed on a flat plate. Boundary layer transition in this situation is investigated by triggering a wave packet, which evolves into a turbulent spot. The development from wave packet to turbulent spot is observed and the interactions of the turbulent spot with the ongoing natural transition and the ensuing turbulent boundary layer are examined. Under this steeply diffusing pressure distribution, strong amplification of primary instabilities prevails. Breakdown to turbulence is instigated near the centerline and propagates transversely along the wave packet until the turbulent region dominates. An extensive calmed region is present behind the spot, which persists well into the surrounding turbulent layer. Celerities of spot leading and trailing edges are presented, as is the spanwise spreading half-angle. Corresponding measurements for spots under a wide range of imposed pressure gradients are compiled and the present results are compared with those of other authors. Resulting correlations for spot propagation parameters are provided for use in computational modeling of the transition region under variable pressure gradients.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Streamwise Pressure Gradient on Turbulent Spot Development
typeJournal Paper
journal volume118
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2840929
journal fristpage737
journal lastpage743
identifier eissn1528-8900
keywordsTurbulence
keywordsPressure gradient
keywordsWave packets
keywordsPressure
keywordsDiffusion (Physics)
keywordsMeasurement
keywordsBoundary layers
keywordsBlades
keywordsBoundary layer turbulence
keywordsFlat plates
keywordsSuction
keywordsComputer simulation AND Compressors
treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 004
contenttypeFulltext


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