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contributor authorD. E. Wilson
contributor authorA. J. Hanford
date accessioned2017-05-08T23:58:13Z
date available2017-05-08T23:58:13Z
date copyrightApril, 1998
date issued1998
identifier issn0889-504X
identifier otherJOTUEI-28665#351_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121338
description abstractA phenomenological model is presented that relates free-stream turbulence to the augmentation of stagnation-point surface flux quantities. The model requires the turbulence intensity, the longitudinal scale of the turbulence, and the energy spectra as inputs for the unsteady velocity at the edge of the near-wall viscous region. The form of the edge velocity contains both pulsations of the incoming flow and oscillations of the streamline. Incompressible results using a single fluctuating component are presented within the stagnation region of a two-dimensional cylinder. The time-averaged Froessling number is determined from the computations. These predictions are compared to existing incompressible experimental data. Additionally, the variations in the surface flux quantities with the longitudinal scale of the incoming free-stream turbulence, the Reynolds number, and the free-stream turbulence intensity are considered.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Unsteady Velocity Formulation for the Edge of the Near-Wall Region
typeJournal Paper
journal volume120
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841413
journal fristpage351
journal lastpage361
identifier eissn1528-8900
keywordsOscillations
keywordsFlow (Dynamics)
keywordsSpectra (Spectroscopy)
keywordsTurbulence
keywordsReynolds number
keywordsComputation AND Cylinders
treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 002
contenttypeFulltext


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