The effect of surface roughness on the mean velocity and skin friction characteristics of a plane turbulent wall jet was experimentally investigated using laser Doppler anemometry. The Reynolds number based on the slot height and exit velocity of the jet was approximately Re = 7500. A 36-grit sheet was used to create a transitionally rough flow (44 < ks+ < 70). Measurements were carried out at downstream distances from the jet exit ranging from 20 to 80 slot heights. Both conventional and momentum-viscosity scaling were used to analyze the streamwise evolution of the flow on smooth and rough walls. Three different methods were employed to estimate the friction velocity in the fully developed region of the wall jet, which was then used to calculate the skin friction coefficient. This paper provides new experimental data for the case of a plane wall jet on a transitionally rough surface and uses it to quantify the effects of roughness on the momentum field. The present results indicate that the skin friction coefficient for the rough-wall case compared to a smooth wall increases by as much as 140%. Overall, the study suggests that for the transitionally rough regime considered in the present study, roughness effects are significant but mostly confined to the inner region of the wall jet.
Skip Nav Destination
e-mail: don.bergstrom@usask.ca
e-mail: david.sumner@usask.ca
e-mail: jim.bugg@usask.ca
Article navigation
November 2011
Research Papers
An Experimental Study of a Turbulent Wall Jet on Smooth and Transitionally Rough Surfaces
D. J. Bergstrom,
D. J. Bergstrom
Department of Mechanical Engineering,
e-mail: don.bergstrom@usask.ca
University of Saskatchewan
, 57 Campus Drive, Saskatoon, SK, S7N 5A9 Canada
Search for other works by this author on:
D. Sumner,
D. Sumner
Department of Mechanical Engineering,
e-mail: david.sumner@usask.ca
University of Saskatchewan
, 57 Campus Drive, Saskatoon, SK, S7N 5A9 Canada
Search for other works by this author on:
J. D. Bugg
J. D. Bugg
Department of Mechanical Engineering,
e-mail: jim.bugg@usask.ca
University of Saskatchewan
, 57 Campus Drive, Saskatoon, SK, S7N 5A9 Canada
Search for other works by this author on:
D. J. Bergstrom
Department of Mechanical Engineering,
University of Saskatchewan
, 57 Campus Drive, Saskatoon, SK, S7N 5A9 Canada
e-mail: don.bergstrom@usask.ca
D. Sumner
Department of Mechanical Engineering,
University of Saskatchewan
, 57 Campus Drive, Saskatoon, SK, S7N 5A9 Canada
e-mail: david.sumner@usask.ca
J. D. Bugg
Department of Mechanical Engineering,
University of Saskatchewan
, 57 Campus Drive, Saskatoon, SK, S7N 5A9 Canada
e-mail: jim.bugg@usask.ca
J. Fluids Eng. Nov 2011, 133(11): 111207 (8 pages)
Published Online: November 11, 2011
Article history
Received:
November 1, 2010
Revised:
September 28, 2011
Online:
November 11, 2011
Published:
November 11, 2011
Citation
Rostamy, N., Bergstrom, D. J., Sumner, D., and Bugg, J. D. (November 11, 2011). "An Experimental Study of a Turbulent Wall Jet on Smooth and Transitionally Rough Surfaces." ASME. J. Fluids Eng. November 2011; 133(11): 111207. https://doi.org/10.1115/1.4005218
Download citation file:
Get Email Alerts
Related Articles
Skin Friction Correlation for Smooth and Rough Wall Turbulent Boundary Layers
J. Fluids Eng (November,2005)
Experimental Investigation of the Turbulent Boundary Layer of Surfaces Coated With Marine Antifoulings
J. Fluids Eng (March,2005)
PIV Study of Shallow Open Channel Flow Over d - and k -Type Transverse Ribs
J. Fluids Eng (August,2007)
Frictional Resistance of Antifouling Coating Systems
J. Fluids Eng (November,2004)
Related Proceedings Papers
Related Chapters
Hydraulic Resistance
Heat Transfer & Hydraulic Resistance at Supercritical Pressures in Power Engineering Applications
Other Components and Variations
Axial-Flow Compressors
The Design and Implement of Remote Inclinometer for Power Towers Based on MXA2500G/GSM
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3