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  4. A Wave-Propagation Based Volume Tracking Method for Compressible Multicomponent Flow in Two Space Dimensions
 
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A Wave-Propagation Based Volume Tracking Method for Compressible Multicomponent Flow in Two Space Dimensions

Resource
Journal of Computational Physics 215(1),219-244
Journal
Journal of Computational Physics
Pages
219-244
Date Issued
2006
Date
2006
Author(s)
KEH-MING SHYUE  
DOI
20060927121127789779
http://ntur.lib.ntu.edu.tw/bitstream/246246/20060927121127789779/1/vof2d.pdf
10.1016/j.jcp.2005.10.030
DOI
20060927121127789779
URI
https://www.scopus.com/record/display.uri?eid=2-s2.0-33645839836&origin=resultslist&sort=plf-f&src=s&sid=44955de48e433d4fe8105345f9fc3319&sot=b&sdt=b&s=TITLE-ABS-KEY%28A+Wave-Propagation+Based+Volume+Tracking+Method+for+Compressible+Multicomponent+Flow+in%29&sl=122&sessionSearchId=44955de48e433d4fe8105345f9fc3319&relpos=0
Abstract
We present a simple volume-of- uid approach to interface tracking for inviscid compressible multicomponent ow problems in two space dimensions. The algorithm uses a uniform Carte- sian grid with some grid cells subdivided by tracked interfaces, approximately aligned with the material interfaces in the ow field. A standard volume-moving procedure that consists of two basic steps: (1) the update of a discrete set of volume fractions from the current time to the next, and (2) the reconstruction of interfaces from the resulting volume fractions, is employed to find the new location of the tracked interfaces in piecewise linear form at the end of a time step. As in the previous work by LeVeque and the author to front tracking based on a surface- moving procedure (J. Comput. Phys., 123 (1996), pp. 354-368), a conservative high-resolution wave propagation method is applied on the resulting slightly nonuniform grid to update all the cell values, while the stability of the method is maintained by using a large time step idea even in the presence of small cells and the use of a time step with respect to the uniform grid cells. We validate our algorithm by performing the simulation of a Mach 1 . 22 shock wave in air over a circular R22 gas bubble, where sensible agreement of some key ow features of the computed solutions are observed when direct comparison of our results are made with the existing experimental and numerical ones appeared in the literature. Other computations are also presented that show the feasibility of the algorithm together with a mixture type of the model equations developed by the author (J. Comput. Phys., 171 (2001), pp. 678-707) for practical multicomponent problems with general compressible materials characterized by a Mie-Gr¨ uneisen form of the equation of state.
Subjects
Volume tracking
Wave propagation method
Multicomponent flows
Mie-Gruneisen equation of state
Impact problem
Type
journal article
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