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contributor authorRichard J. Anthony
contributor authorTerry V. Jones
contributor authorJohn E. LaGraff
date accessioned2017-05-09T00:18:10Z
date available2017-05-09T00:18:10Z
date copyrightApril, 2005
date issued2005
identifier issn0889-504X
identifier otherJOTUEI-28719#241_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132806
description abstractA high-frequency surface heat flux imaging technique was used to investigate bypass transition induced by freestream turbulence. Fundamental experiments were carried out at the University of Oxford using high-density thin film arrays on a flat plate wind tunnel model. Bypass transition was induced by grid-generated turbulence with varying intensities of 2.3%, 4.2%, and 17% with a fixed integral length scale of approximately 12mm. Unique high resolution temporal heat flux images are shown which detail significant differences between unsteady surface heat flux events induced by freestream turbulence and the classical Emmons-type spots which many turbomachinery transition models are based on. The temporal imaging technique presented allows study of unsteady surface heat transfer in detail, and helps elucidate the complex nature of transition in the high-disturbance environment of turbomachinery.
publisherThe American Society of Mechanical Engineers (ASME)
titleHigh Frequency Surface Heat Flux Imaging of Bypass Transition
typeJournal Paper
journal volume127
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1860379
journal fristpage241
journal lastpage250
identifier eissn1528-8900
keywordsTurbulence
keywordsHeat flux
keywordsBoundary layers
keywordsImaging AND Heat transfer
treeJournal of Turbomachinery:;2005:;volume( 127 ):;issue: 002
contenttypeFulltext


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