The Limitations of Using “Ra” to Describe Surface Roughness

Author:

Goodhand Martin N.1,Walton Karl2,Blunt Liam2,Lung Hang W.3,Miller Robert J.1,Marsden Reg3

Affiliation:

1. Whittle Laboratory, University of Cambridge, Cambridge CB2 3BU, UK e-mail:

2. Centre for Innovative Manufacturing in Advanced Metrology, University of Huddersfield, Huddersfield HD1 3DH, UK e-mail:

3. Rolls-Royce Plc, Derby DE24 8BJ, UK e-mail:

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/λ. To demonstrate the relationship, wake traverses were undertaken downstream of an aerofoil with various polished surfaces. The admissible roughness Reynolds number (ρ1u1Ra/μ1) 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

ASME International

Subject

Mechanical Engineering

Reference10 articles.

1. A Review of Surface Roughness Effects in Gas Turbines;ASME J. Turbomach.,2010

2. Admissible Roughness in Turbomachines,2015

3. Feindt, E. G., 1957, “Untersuchungen uber die Abhangigkeit des Umschlages laminar-turbulent von der Oberflachenrauhigkeit und der Druckverteilung,” Diss. Braunschweig, Jb. 1956 Schiffbautechn. Gessellschaft 50, pp. 180–203.

4. Boundary Layer Transition at Mach 3.12 With and Without Single Roughness Element,1954

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