運動激波和氣泡串相互作用的初步數(shù)值模擬

1、 448 計 算 物 理 第 21 卷 參 考 文 獻 1 Fedkiw R , Aslam T , Merriman B , Osher S. A Non 2oscillatory Eulerian Approach to Interfaces in Multimaterial Flows J . J Comput Phys ,1999 ,152 :457 - 492. 2 Harten A. High resolution schemes for hyper conservation laws J . J Comput Phys , 1983 , 49 : 357 - 393. 3 Shu

2、 C. Essentially non2oscillatory and weighted essentially non 2oscillatory schemes for hyperbolic conservation laws R . NASA CR2 972206253. 1997. 4 劉儒勛 ,王志峰 . 數(shù)值模擬方法和運動界面追蹤 M . 合肥 : 中國科學(xué)技術(shù)大學(xué)出版社 ,2001. 5 Fedkiw R , Marquina A , Merriman B. An isobaric fix for the overheating problem in multimaterial c

3、ompressible flows J . J Comput Phys , 1999 , 148 : 545 - 578. Numerical Studies of Moving Shock Interacting with Consecutive Helium Bubbles CHEN Fei , ZHANG Meng2ping , XU Sheng2li ( Dept . of Mechanics and Mech . Egr. , University of Science and Technology of China , Hefei 230027 , China Abstract :

4、 The numerical simulations is carried out on interface with large deformation induced by interaction between a moving shock and Helium bubbles. The high performance of the level set method coupling with GFM( ghost fluid method method was demonstrated. Upwind TVD scheme was used to solve Eulerian equ

5、ation for flowfield ,and 5th WENO scheme was used to solve level set equation for fluid interfaces track2 ing. GFM was applied to deal with the interface boundary. Example in Ref. 1 was used to validate our codes. Finally ,the results were obtained on moving shock interacting with helium bubbles including the bubbles evolution. The results indicate that multi 2interface can be perfectly tracked by extension of level set equation for multi2fluid interfaces. Key words : level set method ; upwi