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Shapes, stability and hysteresis of rotating and charged axisymmetric drops in vacuum
- Publication Year :
- 2018
- Publisher :
- AIP Publishing, 2018.
-
Abstract
- The behavior of rotating and/or charged drops is a classic problem in fluid mechanics with a multitude of industrial applications. Theoretical studies of such liquid drops have also provided important insights into fundamental physical processes across nuclear and astrophysical lengthscales. However, the full nonlinear dynamics of these drops are only just beginning to be uncovered by experiments. These nonlinear effects are manifest in the high sensitivity of the breakup mechanisms to small perturbations of the initial drop shape and in observations of hysteresis in the transition between different drop shape families. This paper investigates the equilibrium shapes and stability of charged and rotating drops in a vacuum with an energy minimization method applied to spheroidal shapes and with numerical simulations using a finite-difference, level-set method. A good working formula for the stability limit of these drops is given by Lmax = 1.15 − 0.59x − 0.56x2, where L is the dimensionless angular momentum and x is the charge fissility parameter. These methods also provide a firm explanation for the hysteresis of rotating and charged drops.
- Subjects :
- DYNAMICS
Angular momentum
Technology
Fluids & Plasmas
Computational Mechanics
Rotational symmetry
WATER DROPS
Mechanics
01 natural sciences
ELECTRIC-FIELD
09 Engineering
010305 fluids & plasmas
Physics::Fluid Dynamics
CONDENSATION
Physics, Fluids & Plasmas
DEFORMATION
0103 physical sciences
010306 general physics
01 Mathematical Sciences
LEVEL SET METHODS
Fluid Flow and Transfer Processes
Physics
BREAK-UP
Science & Technology
02 Physical Sciences
Mechanical Engineering
Fluid mechanics
Condensed Matter Physics
Breakup
Nonlinear system
Hysteresis
Mechanics of Materials
LIQUID-DROPS
Physical Sciences
Two-phase flow
INJECTION
DISINTEGRATION
Dimensionless quantity
Subjects
Details
- Database :
- OpenAIRE
- Accession number :
- edsair.doi.dedup.....678ce517921f03ad81ec4e22467f9b8b