An experimental investigation was conducted to quantify the characteristics of the turbulent boundary layer flows over a dimpled surface in comparison to those over a conventional flat plate. In addition to measuring surface pressure distributions to determine the friction factors of the test plates and to map the surface pressure inside the dimple cavity, a high-resolution digital particle image velocimetry (PIV) system was used to achieve detailed flow field measurements to quantify the characteristics of the turbulent boundary layer flows over the test plates and the evolution of the unsteady vortex structures inside the dimple cavity at the middle of the dimpled test plate. It was found that the friction factor of the dimpled plate would be about 30–80% higher than that of the flat plate, depending on the Reynolds number of the test cases. In comparison with those over a conventional flat surface, the flow characteristics of the turbulent boundary layer flows over the dimpled surface were found to be much more complicated with much stronger near-wall Reynolds stress and higher turbulence kinetic energy (TKE) levels, especially in the region near the back rims of the dimples. Many interesting flow features over the dimple surface, such as the separation of oncoming boundary layer flow from the dimpled surface when passing over the dimple front rim, the formation and periodic shedding of unsteady Kelvin–Helmholtz vortices in the shear layer over the dimple, the impingement of the high-speed incoming flow onto the back rim of the dimple, and the subsequent generation of strong upwash flow in the boundary flow to promote the turbulent mixing over the dimpled surface, were revealed clearly and quantitatively from the PIV measurement results. The quantitative measurement results are believed to be the first of its nature, which depict a vivid picture about the unique flow features over dimpled surfaces and their correlations with the enhanced heat transfer performance reported in previous studies.
Skip Nav Destination
Article navigation
February 2016
Research-Article
An Experimental Investigation on the Characteristics of Turbulent Boundary Layer Flows Over a Dimpled Surface
Wenwu Zhou,
Wenwu Zhou
Department of Aerospace Engineering,
Iowa State University,
Ames, IA 50011
Iowa State University,
Ames, IA 50011
Search for other works by this author on:
Yu Rao,
Yu Rao
Gas Turbine Research Institute,
School of Mechanical Engineering,
Shanghai Jiao Tong University,
Shanghai 200240, China
e-mail: yurao@sjtu.edu.cn
School of Mechanical Engineering,
Shanghai Jiao Tong University,
Shanghai 200240, China
e-mail: yurao@sjtu.edu.cn
Search for other works by this author on:
Hui Hu
Hui Hu
Search for other works by this author on:
Wenwu Zhou
Department of Aerospace Engineering,
Iowa State University,
Ames, IA 50011
Iowa State University,
Ames, IA 50011
Yu Rao
Gas Turbine Research Institute,
School of Mechanical Engineering,
Shanghai Jiao Tong University,
Shanghai 200240, China
e-mail: yurao@sjtu.edu.cn
School of Mechanical Engineering,
Shanghai Jiao Tong University,
Shanghai 200240, China
e-mail: yurao@sjtu.edu.cn
Hui Hu
1Corresponding author.
Contributed by the Fluids Engineering Division of ASME for publication in the JOURNAL OF FLUIDS ENGINEERING. Manuscript received March 15, 2015; final manuscript received July 29, 2015; published online September 10, 2015. Assoc. Editor: Mark F. Tachie.
J. Fluids Eng. Feb 2016, 138(2): 021204 (13 pages)
Published Online: September 10, 2015
Article history
Received:
March 15, 2015
Revised:
July 29, 2015
Citation
Zhou, W., Rao, Y., and Hu, H. (September 10, 2015). "An Experimental Investigation on the Characteristics of Turbulent Boundary Layer Flows Over a Dimpled Surface." ASME. J. Fluids Eng. February 2016; 138(2): 021204. https://doi.org/10.1115/1.4031260
Download citation file:
Get Email Alerts
Effects of Tire Attributes on the Aerodynamic Performance of a Generic Car–Tire Assembly
J. Fluids Eng (January 2025)
Related Articles
Effect of Tip Gap Size on the Tip Flow Structure and Turbulence Generation in a Low Reynolds Number Compressor Cascade
J. Fluids Eng (November,2024)
An Experimental Study on the Influence of Vortex Generators on the Shock-Induced Boundary Layer Separation at M = 1.4
J. Appl. Mech (July,2009)
Semi-circular Rods Used to Control Turbulent Boundary Layer Separation at Cylindrical Surface
J. Fluids Eng (May,2006)
Related Proceedings Papers
Related Chapters
Cavitating Structures at Inception in Turbulent Shear Flow
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Pulsating Supercavities: Occurrence and Behavior
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Extended Surfaces
Thermal Management of Microelectronic Equipment, Second Edition