The Limitations of Using “Ra†to Describe Surface RoughnessSource: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 010::page 101003Author:Goodhand, Martin N.
,
Walton, Karl
,
Blunt, Liam
,
Lung, Hang W.
,
Miller, Robert J.
,
Marsden, Reg
DOI: 10.1115/1.4032280Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Current 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.
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contributor author | Goodhand, Martin N. | |
contributor author | Walton, Karl | |
contributor author | Blunt, Liam | |
contributor author | Lung, Hang W. | |
contributor author | Miller, Robert J. | |
contributor author | Marsden, Reg | |
date accessioned | 2017-05-09T01:34:09Z | |
date available | 2017-05-09T01:34:09Z | |
date issued | 2016 | |
identifier issn | 0889-504X | |
identifier other | turbo_138_10_101003.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/162770 | |
description abstract | Current 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | The Limitations of Using “Ra†to Describe Surface Roughness | |
type | Journal Paper | |
journal volume | 138 | |
journal issue | 10 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4032280 | |
journal fristpage | 101003 | |
journal lastpage | 101003 | |
identifier eissn | 1528-8900 | |
tree | Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 010 | |
contenttype | Fulltext |