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contributor authorA. J. Hanford
contributor authorD. E. Wilson
date accessioned2017-05-08T23:45:53Z
date available2017-05-08T23:45:53Z
date copyrightJanuary, 1994
date issued1994
identifier issn0889-504X
identifier otherJOTUEI-28634#46_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114585
description abstractA phenomenological model is proposed that relates the effect of free-stream turbulence to the increase in stagnation point heat transfer. The model requires both turbulence intensity and energy spectra as inputs to the unsteady velocity at the edge of the boundary layer. The form of the edge velocity contains both a pulsation of the incoming flow and an oscillation of the streamlines. The incompressible unsteady and time-averaged boundary layer response is determined by solving the momentum and energy equations. The model allows for arbitrary two-dimensional geometry; however, results are given only for a circular cylinder. The time-averaged Nusselt number is determined theoretically and compared to existing experimental data.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of a Turbulent Wake on the Stagnation Point: Part II—Heat Transfer Results
typeJournal Paper
journal volume116
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2928277
journal fristpage46
journal lastpage56
identifier eissn1528-8900
keywordsWake turbulence
keywordsHeat transfer
keywordsTurbulence
keywordsBoundary layers
keywordsCircular cylinders
keywordsEquations
keywordsGeometry
keywordsOscillations
keywordsMomentum
keywordsFlow (Dynamics) AND Spectra (Spectroscopy)
treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 001
contenttypeFulltext


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