Modes and break periods of electrowetting liquid bridge

Mohsen Torabi, Ahmed A. Hemeda, James W. Palko, Yu Feng, Yong Cao, and Yanbao Ma
Phys. Rev. E 100, 033102 – Published 11 September 2019

Abstract

In this paper, we propose a microscale liquid oscillator using electrowetting-on-dielectric (EWOD). Specifically, a mesoscale liquid bridge (LB) between two horizontal surfaces with EWOD is considered. When EWOD is applied, the solid surface becomes more hydrophilic, and hence the contact angle (CA) is reduced. Following the activation of EWOD, the LB can remain connected or it can break into either symmetric or asymmetric shapes depending on the initial liquid volume and wettability of the two surfaces. The LB dynamics activated by EWOD is studied using the multibody dissipative particle dynamics (MDPD) method. Our numerical results show that the behavior of an LB under EWOD can be interpreted via three modes. In the first mode, the LB does not break after applying EWOD. In the second mode, the LB breaks and does not reform. The third mode happens when, depending on the interplay of the volume of the liquid and CA manipulation, the LB continuously breaks, recoils, and reforms. For asymmetric cases, it was observed that the LB may completely detach from one surface and may not reform. It was also observed that decreasing the wettability of a surface, for cases with a continuous breaking and reformation behavior, increases the connecting time interval and decreases the breaking time interval in one break-reform cycle. The results provided in this investigation facilitate fundamental understanding of LB dynamics and their application for the design of microscale liquid oscillators using EWOD.

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  • Received 10 May 2019
  • Revised 21 July 2019

DOI:https://doi.org/10.1103/PhysRevE.100.033102

©2019 American Physical Society

Physics Subject Headings (PhySH)

Fluid Dynamics

Authors & Affiliations

Mohsen Torabi1,*, Ahmed A. Hemeda1,2,*, James W. Palko1, Yu Feng3, Yong Cao3, and Yanbao Ma1,†

  • 1School of Engineering, University of California, Merced, California 95343, USA
  • 2Aerospace Engineering Department, Cairo University, 12613 Egypt
  • 3Harbin Institute of Technology, Shenzhen, Guangdong 518055, People's Republic of China

  • *These authors contributed equally to this work.
  • yma5@ucmerced.edu

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Vol. 100, Iss. 3 — September 2019

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