4.7 Article

Superhydrophobic drag reduction in high-speed towing tank

Journal

JOURNAL OF FLUID MECHANICS
Volume 908, Issue -, Pages -

Publisher

CAMBRIDGE UNIV PRESS
DOI: 10.1017/jfm.2020.872

Keywords

turbulence control; drag reduction; MEMS; NEMS

Funding

  1. DARPA [HR0011-15-2-0021]
  2. NSF [1336966, 1720499]
  3. ONR [N000141110503]
  4. Directorate For Engineering [1336966] Funding Source: National Science Foundation
  5. Directorate For Engineering
  6. Div Of Civil, Mechanical, & Manufact Inn [1720499] Funding Source: National Science Foundation
  7. Div Of Chem, Bioeng, Env, & Transp Sys [1336966] Funding Source: National Science Foundation

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This study demonstrates that under controlled flow conditions, the reduction in skin-friction drag can be achieved by using specific microtrench SHPo surfaces. The width of the trenches non-dimensionalized to the viscous length scale is found to govern the extent of skin-friction drag reduction.
As far as plastron is sustained, superhydrophobic (SHPo) surfaces are expected to reduce skin-friction drag in any flow conditions including large-scale turbulent boundary-layer flows of marine vessels. However, despite many successful drag reductions reported using laboratory facilities, the plastron on SHPo surfaces was persistently lost in high-Reynolds-number flows on open water, and no reduction has been reported until a recent study using certain microtrench SHPo surfaces underneath a boat (Xu et al., Phys. Rev. Appl., vol. 13, no. 3, 2020, 034056). Since scientific studies with controlled flows are difficult with a boat on ocean water, in this paper we test similar SHPo surfaces in a high-speed towing tank, which provides well-controlled open-water flows, by developing a novel 0.7 m x 1.4 m towing plate, which subjects a 4 cm x 7 cm sample to the high-Reynolds-number flows of the plate. In addition to the 7 cm long microtrenches, trenches divided into two in length are also tested and reveal an improvement. The skin-friction drag ratio relative to a smooth surface is found to be decreasing with increasing Reynolds number, down to 73% (i.e. 27% drag reduction) at Re-x similar to 8 x 10(6), before starting to increase at higher speeds. For a given gas fraction, the trench width non-dimensionalized to the viscous length scale is found to govern the drag reduction, in agreement with previous numerical results.

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