Scaling Hydrodynamic Boundary Conditions of Microstructured Surfaces in the Thin Channel Limit.

Langmuir

Department of Chemical and Biomolecular Engineering, Johns Hopkins University, Baltimore, Maryland 21218, United States.

Published: March 2016

AI Article Synopsis

  • A unified understanding of how nano- and microscale surface features affect fluid interactions, especially in hydrodynamics, remains incomplete.
  • The study focuses on the behavior of viscous silicone oil between a flat surface and various hexagonal arrays of microsized cylindrical posts, noting that the structure sizes are much larger than the measurement separation range.
  • The research identifies three distinct regimes of hydrodynamic drag based on the distance between surfaces, revealing that traditional models can't fully explain the behavior observed in close proximity to the microposts.

Article Abstract

Despite its importance in many applications and processes, a complete and unified view on how nano- and microscale asperities influence hydrodynamic interactions has yet to be reached. In particular, the effects of surface structure can be expected to become more dominant when the length scale of the asperities or textures becomes comparable to that of the fluid flow. Here we analyze the hydrodynamic drainage of a viscous silicone oil squeezed between a smooth plane and a surface decorated with hexagonal arrays of lyophilic microsized cylindrical posts. For all micropost arrays studied, the periodicity of the structures was much larger than the separation range of our measurements. In this thin channel geometry, we find the hydrodynamic drainage and separation forces for the micropost arrays cannot be fully described by existing boundary condition models for interfacial slip or a no-slip shifted plane. Instead, our results show that the influence of the microposts on the hydrodynamic drag exhibits three distinct regimes as a function of separation. For large separations, a no slip boundary condition (Reynolds theory) is observed for all surfaces until a critical (intermediate) separation, below which the position of the no-slip plane scales with surface separation until reaching a maximum, just before contact. Below this separation, a sharp decrease in the no-slip plane position then suggests that a boundary condition of a smooth surface is recovered at contact.

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Source
http://dx.doi.org/10.1021/acs.langmuir.5b04134DOI Listing

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