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Superhydrophobic turbulent drag reduction as a function of surface grating parameters

Published online by Cambridge University Press:  23 April 2014

Hyungmin Park*
Affiliation:
Mechanical and Aerospace Engineering Department, University of California at Los Angeles (UCLA), Los Angeles, CA 90095, USA
Guangyi Sun*
Affiliation:
Mechanical and Aerospace Engineering Department, University of California at Los Angeles (UCLA), Los Angeles, CA 90095, USA
Chang-Jin “CJ” Kim*
Affiliation:
Mechanical and Aerospace Engineering Department, University of California at Los Angeles (UCLA), Los Angeles, CA 90095, USA
*
Present address: Department of Mechanical & Aerospace Engineering, Seoul National University, Seoul 151-744, Korea.
Present address: Institute of Robotics and Automatic Information System, Nankai University, Tianjin Key Laboratory of Intelligent Robotics, Tianjin 300071, China.
§Email address for correspondence: [email protected]

Abstract

Despite the confirmation of slip flows and successful drag reduction (DR) in small-scaled laminar flows, the full impact of superhydrophobic (SHPo) DR remained questionable because of the sporadic and inconsistent experimental results in turbulent flows. Here we report a systematic set of bias-free reduction data obtained by measuring the skin-friction drags on a SHPo surface and a smooth surface at the same time and location in a turbulent boundary layer (TBL) flow. Each monolithic sample consists of a SHPo surface and a smooth surface suspended by flexure springs, all carved out from a $2.7 \times 2.7 {\mathrm{mm}}^{2}$ silicon chip by photolithographic microfabrication. The flow tests allow continuous monitoring of the plastron on the SHPo surfaces, so that the DR data are genuine and consistent. A family of SHPo samples with precise profiles reveals the effects of grating parameters on turbulent DR, which was measured to be as much as ${\sim }75\, \%$.

Type
Papers
Copyright
© 2014 Cambridge University Press 

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Park et al. supplementary movie

Comparative displacement of a SHPo surface and a smooth surface measured in in a turbulent boundary layer flow (Reτ ~ 250) – 50× slower. It is clearly seen that the SHPo surface (50 μm pitch and 90% GF) is dragged less than a smooth counterpart in a turbulent flow which indicates a skin-friction drag reduction.

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