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One-dimensional dynamics of nearly unstable axisymmetric liquid bridges

Perales Perales, José Manuel and Vega de Prada, José Manuel (2010) One-dimensional dynamics of nearly unstable axisymmetric liquid bridges. Physics of Fluids, 22 (11). 112114-1-112114-10. ISSN 1070-6631

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Item Type:Article
Authors/Creators:
Creators NameCreators email (if known)
Perales Perales, José Manuel
Vega de Prada, José Manuel
Title:One-dimensional dynamics of nearly unstable axisymmetric liquid bridges
Publisher:American Institute of Physics
Journal/Publication Title:Physics of Fluids
Date:November 2010
Volume:22
Number:11
Department:Mathematical Fundamentals of Aeronautics Technology
Faculty:E.T.S.I. Aeronautical (UPM)
Creative Commons licenses:Recognition - No derivative works - No commercial
Item ID:5959
Subjects:Aeronautics

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Official URL: http://pof.aip.org/resource/1/phfle6/v22/i11/p112114_s1?isAuthorized=no

Abstract

A general one-dimensional model is considered that describes the dynamics of slender, axisymmetric, noncylindrical liquid bridges between two equal disks. Such model depends on two adjustable parameters and includes as particular cases the standard Lee and Cosserat models. For slender liquid bridges, the model provides sufficiently accurate results and involves much easier and faster calculations than the full three-dimensional model. In particular, viscous effects are easily accounted for. The one-dimensional model is used to derive a simple weakly nonlinear description of the dynamics near the instability limit. Small perturbations of marginal instability conditions are also considered that account for volume perturbations, nonequality of the supporting disks, and axial gravity. The analysis shows that the dynamics breaks the reflection symmetry on the midplane between the supporting disks. The weakly nonlinear evolution of the amplitude of the perturbation is given by a Duffing equation, whose coefficients are calculated in terms of the slenderness as a part of the analysis and exhibit a weak dependence on the adjustable parameters of the one-dimensional model. The amplitude equation is used to make quantitative predictions of both the (first stage of) breakage for unstable configurations and the (slow) dynamics for stable configurations.

Item Type:Article
Subjects:Aeronautics
Código ID:5959
Depositado Por:Memoria de Investigacion 2
Depositado el:09 Feb 2011 15:32
Last Modified:09 Feb 2011 15:32

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