2004
DOI: 10.1016/j.jnnfm.2004.06.012
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A numerical method for solving three-dimensional generalized Newtonian free surface flows

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Cited by 39 publications
(41 citation statements)
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“…The value θ UU in Eq. (36) refers to the liquid volume fraction in the second upwind cell relative to face f. The original HRIC scheme further blends the interpolated values given by the scheme (35), with the UDS scheme, when the interface is not parallel to the cell's face, and when the local Courant number exceeds the threshold value 0.3. These corrections to the interpolated flux of the liquid volume aim at avoiding an artificial alignment of the interface with the numerical grid, as well as convergence issues.…”
Section: Algebraic Advection Schemementioning
confidence: 99%
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“…The value θ UU in Eq. (36) refers to the liquid volume fraction in the second upwind cell relative to face f. The original HRIC scheme further blends the interpolated values given by the scheme (35), with the UDS scheme, when the interface is not parallel to the cell's face, and when the local Courant number exceeds the threshold value 0.3. These corrections to the interpolated flux of the liquid volume aim at avoiding an artificial alignment of the interface with the numerical grid, as well as convergence issues.…”
Section: Algebraic Advection Schemementioning
confidence: 99%
“…the flow of the surrounding air is omitted). This method was used to simulate the extrudate swell and jet buckling phenomena for the generalized Newtonian fluid model [34,35], and for various viscoelastic constitutive models [36][37][38][39][40][41]. In the level-set method, the position of the interface (or the free surface) is represented with a level-set function that varies continuously across the interface [42].…”
Section: Introductionmentioning
confidence: 99%
“…However, the level set surface generated by this method does not preserve temporal coherence due to the slow motion of the liquid. In computational physics literature, there are several papers using variations of generalized simplified MAC (GENSMAC) method to simulate viscous jet buckling in arbitrary 2D/3D domains with explicit [11][12][13] and implicit [14] free surface boundary conditions.…”
Section: Related Workmentioning
confidence: 99%
“…5). In our simulations of this problem, we use values for H, D and physical parameters consistent with the conditions described by Tomé et al [13].…”
Section: Jet Bucklingmentioning
confidence: 99%
“…Reynolds são frequentes (por exemplo as aplicações em [162,161] por Prudhomme e Oden [131]. Outros estudos recentes têm sido realizados na estabilidade de esquemas implícitos aplicados às equações de Navier-Stokes: para fórmulas de diferenças atrasadas (backward dierentiation formulas) [83], para uma discretização totalmente implícita das equações de Navier-Stokes utilizando o método de Euler implícito [166], e para esquemas de Runge-Kutta [111].…”
Section: Esquemas Implícitos Na Metodologia Gensmacunclassified