2007
DOI: 10.1016/j.jcp.2007.04.028
|View full text |Cite
|
Sign up to set email alerts
|

An isochoric domain deformation method for computing steady free surface flows with conserved volumes

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2009
2009
2016
2016

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(3 citation statements)
references
References 15 publications
0
3
0
Order By: Relevance
“…From a computational standpoint, the moving internal boundaries present a numerical challenge, and two classes of methods have been developed to meet it: interface tracking and interface capturing [2]. The former deploys grid points or markers on the interface that track it each time step [3][4][5]. The latter uses an auxiliary scalar field that distinguishes the fluid components.…”
Section: Introductionmentioning
confidence: 99%
“…From a computational standpoint, the moving internal boundaries present a numerical challenge, and two classes of methods have been developed to meet it: interface tracking and interface capturing [2]. The former deploys grid points or markers on the interface that track it each time step [3][4][5]. The latter uses an auxiliary scalar field that distinguishes the fluid components.…”
Section: Introductionmentioning
confidence: 99%
“…To address the latter, a number of pioneering studies (Epureanu et al, 2002;Anttonen et al, 2003Anttonen et al, , 2005Feng and Soulaïmani, 2007;Liberge et al, 2008) endeavored to adapt Eulerian-Lagrangian dynamic mesh adaptation methods, that are commonly used in CFD models of aeroelasticity (Batina, 1990;Farhat et al, 1998;Blom, 2000;Schuster et al, 2003;Ishihara and Yoshimura, 2005;Hsu and Chang, 2007;Xie et al, 2007;Braun et al, 2008;Roszak et al, 2009). To address the latter, a number of pioneering studies (Epureanu et al, 2002;Anttonen et al, 2003Anttonen et al, , 2005Feng and Soulaïmani, 2007;Liberge et al, 2008) endeavored to adapt Eulerian-Lagrangian dynamic mesh adaptation methods, that are commonly used in CFD models of aeroelasticity (Batina, 1990;Farhat et al, 1998;Blom, 2000;Schuster et al, 2003;Ishihara and Yoshimura, 2005;Hsu and Chang, 2007;Xie et al, 2007;Braun et al, 2008;Roszak et al, 2009).…”
Section: Lagrangian-ulerian Methods and Deformable Gridsmentioning
confidence: 99%
“…For steady state flows, one can solve the problem by the domain deformation method [26,91] or even simplify the problem to Laplace equations [55,64] by neglecting viscous effects.…”
Section: Computational Backgroundmentioning
confidence: 99%