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contributor authorGoodhand, Martin N.
contributor authorWalton, Karl
contributor authorBlunt, Liam
contributor authorLung, Hang W.
contributor authorMiller, Robert J.
contributor authorMarsden, Reg
date accessioned2017-05-09T01:34:09Z
date available2017-05-09T01:34:09Z
date issued2016
identifier issn0889-504X
identifier otherturbo_138_10_101003.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162770
description abstractCurrent criteria used to determine whether rough surfaces affect skin friction typically rely on a single amplitude parameter to characterize the roughness. The most commonly used criteria relate the centerline averaged roughness, Ra, to an equivalent sandgrain roughness size, ks. This paper shows that such criteria are oversimplified and that Ra/ks is dependent on the roughness topography, namely, the roughness slope defined as the roughness amplitude normalized by the distance between roughness peaks, Ra/خ». To demonstrate the relationship, wake traverses were undertaken downstream of an aerofoil with various polished surfaces. The admissible roughness Reynolds number (دپ1u1Ra/خ¼1) at which the drag rose above the smooth blade case was determined. The results were used to demonstrate a 400% variation in Ra/ks over the roughness topographies tested. The relationship found held for all cases tested, except those where the roughness first initiated premature transition at the leading edge. In these cases, where the roughness was more typical of eroded aerofoils, the drag was found to rise earlier.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Limitations of Using “Raâ€‌ to Describe Surface Roughness
typeJournal Paper
journal volume138
journal issue10
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4032280
journal fristpage101003
journal lastpage101003
identifier eissn1528-8900
treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 010
contenttypeFulltext


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