DocumentCode :
2759593
Title :
Numerical Study on Splash Conditions of an Integrated Droplet-type Divertor
Author :
Xiao-yong Luo ; Ming-Jiu Ni ; Ying, Alice ; Abdou, M.
Author_Institution :
California Univ., Los Angeles, CA
fYear :
2005
fDate :
Sept. 2005
Firstpage :
1
Lastpage :
4
Abstract :
A level set method combined with the second-order RKCN projection method for the multiphase incompressible flow was developed and applied to a free surface flow divertor concept. Crank-Nicholson method for the diffusion term was used to eliminate the numerical viscous stability restriction. The high order ENO scheme was used for the convective term to guarantee the accuracy of the method. The results show the numerical methodology is successful in modeling the hydrodynamics of the multiphase flow even if severe surface deformation occurs. Through performing the different conditions of the droplets like size, velocity, inject angle, we give a detail description on the splash conditions of the integrated droplet-type divertor
Keywords :
diffusion; drops; flow simulation; fusion reactor divertors; fusion reactor theory; hydrodynamics; multiphase flow; Crank-Nicholson method; convective term; diffusion; droplet inject angle; droplet size; droplet velocity; free surface flow divertor; high order ENO scheme; hydrodynamics; integrated droplet-type divertor; level set method; multiphase incompressible flow; numerical viscous stability restriction; second-order RKCN projection method; splash conditions; surface deformation; Deformable models; Equations; Hydrodynamics; Level set; Numerical stability; Plasma materials processing; Plasma temperature; Spraying; Surface tension; Thermal conductivity; Level set method; RKCN projection method; divertor; non-splash; spray droplet;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fusion Engineering 2005, Twenty-First IEEE/NPS Symposium on
Conference_Location :
Knoxville, TN
Print_ISBN :
0-4244-0150-X
Electronic_ISBN :
0-4244-0150-X
Type :
conf
DOI :
10.1109/FUSION.2005.252906
Filename :
4018940
Link To Document :
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