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Interaction between a vortex and a turbulent boundary layer - Part I: Mean flow evolution and turbulence properties

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:54:02Z
date available2017-09-04T16:54:02Z
date copyright01/01/1987
date issued1987
identifier otherWXHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/117459
description abstractAn experimental study was conducted to examine the interaction between a single weak streamwise vortex and a two-dimensional turbulent boundary layer. Attention was focused on characterizing the effect of the boundary layer on the vortex, including the effects of a moderate adverse pressure gradient. Rapid growth of the vortex core was observed, and a flattening of the core shape occurred when the dimension of the core radius became comparable to the distance of the vortex center from the surface. Adverse pressure gradients caused an increase in the rate of core growth, and therefore, a stronger distortion of the core shape. Measurements of surface skin friction beneath the vortex and some of the Reynolds stresses are presented.
languageEnglish
titleNASA-TM-88361num
titleInteraction between a vortex and a turbulent boundary layer - Part I: Mean flow evolution and turbulence propertiesen
typestandard
page47
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1987
contenttypefulltext
subject keywordsDELTA WINGS
subject keywordsFLOW VELOCITY
subject keywordsPRESSURE GRADIENTS
subject keywordsREYNOLDS STRESS
subject keywordsSHEAR STRESS
subject keywordsSKIN FRICTION
subject keywordsTHREE DIMENSIONAL FLOW
subject keywordsTURBULENT BOUNDARY LAYER
subject keywordsVORTEX BREAKDOWN
subject keywordsVORTEX GENERATORS
subject keywordsVORTICITY
subject keywordsWIND TUNNEL TESTS


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