Bulletin of the American Physical Society
71st Annual Meeting of the APS Division of Fluid Dynamics
Volume 63, Number 13
Sunday–Tuesday, November 18–20, 2018; Atlanta, Georgia
Session Q12: Drops: Electric Field Effects
12:50 PM–3:26 PM,
Tuesday, November 20, 2018
Georgia World Congress Center
Room: B217
Chair: Yuan-Nan Young, New Jersey Institute of Technology
Abstract ID: BAPS.2018.DFD.Q12.8
Abstract: Q12.00008 : Influence of Capillary Number and Substrate Curvature on Taylor Cone Formation in Thin Conductive Viscous Films*
2:21 PM–2:34 PM
Presenter:
Theodore G. Albertson
(California Institute of Technology, 1200 E. California Blvd., MC 128-95, Pasadena, CA 91125)
Authors:
Theodore G. Albertson
(California Institute of Technology, 1200 E. California Blvd., MC 128-95, Pasadena, CA 91125)
Sandra Troian
(California Institute of Technology, 1200 E. California Blvd., MC 128-95, Pasadena, CA 91125)
We previously demonstrated by direct numerical simulation that Taylor cone formation in liquid metals confined between parallel substrates held at constant voltage difference proceeds by a self-similar process irrespective of the Reynolds number Re. The power law exponents characterizing the Maxwell and capillary pressure at the conical tip vary smoothly with Re at fixed capillary number Ca. The observed behavior smoothly bridges the inviscid prediction by Zubarev (2001) to the Stokes flow prediction by Fontelos, Kindelan and Vantzos (2008). In this work, we focus on the thin film limit in axisymmetric geometry and explore two additional aspects, namely the influence of Ca on surface excitation and growth and the influence of substrate curvature on single and multimode protrusions. Generally speaking, we find that increasing Ca at fixed Re for flow on curved surfaces generates undulations whose wavelength closely approximate the fastest growing mode associated with the fundamental planar linear instability. More interestingly, certain types of substrate curvature trigger sinusoidal traveling waves with the potential for both on- and off-axis emission.
*The authors gratefully acknowledge financial support from a 2014 NASA Space Technology Research Fellowship (TGA).
To cite this abstract, use the following reference: http://meetings.aps.org/link/BAPS.2018.DFD.Q12.8
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