[1] Padilla J F, Tseng K C, Boyd I D. Analysis of entry vehicle aerothermodynamics using the direct simulation Monte Carlo mehod, AIAA-2005-4681. Reston: AIAA, 2005.
[2] Moss J N, Glass C E, Greene F A. DSMC simulation of apollo capsule aerodynamics for hypersonic rarefied conditions, AIAA-2006-3577. Reston: AIAA, 2006.
[3] Ivanov M S, Markelov G N, Gimelshein S F. High-altitude capsule aerodynamics with real gas effects[J]. Journal of Spacecraft and Rockets, 1998, 35(1): 16-22.
[4] Kim M G, Kim H S. A parallel cell based DSMC method with dynamic load balancing using unstructured adaptive meshes, AIAA-2003-1033. Reston: AIAA, 2003.
[5] Laux M. Optimization and parallelization of the DSMC method on un-structured grids, AIAA-1997-2512. Reston: AIAA, 1997.
[6] Matsumoto Y, Tokumasu T. Parallel computing of diatomic molecular rarefied gas flows[J]. Parallel Computing, 1997, 23(9): 1249-1260.
[7] Dietrich S, Boyd I D. Scalar and parallel optimized implementation of the direct simulation Monte Carlo method[J]. Journal of Computational Physics, 1996, 126(2): 328-342.
[8] Wu J S, Tseng K C. Parallel DSMC method using dynamic domain decomposition[J].International Journal for Numerical Methods in Engineering, 2005, 63(1): 37-76.
[9] Wu J S, Tseng K C, Yang T J. Parallel implementation of DSMC using unstructured mesh[J]. International Journal of Computational Fluid Dynamics, 2003, 17(5): 405-422.
[10] Wu J S, Tseng K C. Concurrent DSMC method using dynamic domain decomposition//23rd International Symposium on Rarefied Gas Dynamics, 2003: 406-413.
[11] LeBeau G J. A parallel implementation of the direct simulation Monte Carlo method[J]. Computer Methods in Applied Mechanics and Engineering, 1999, 174(3): 319-337.
[12] Ivanov M S, Markelov G N, Gimelshein S F. Statistical simulation of reactive rarefied flows:numerical approach and applications, AIAA-1998-2669. Reston: AIAA, 1998.
[13] Otahal T J, Gallis M A, Bartel T J. An investigation of two-dimensional CAD generated models with body decoupled cartesian grids for DSMC, AIAA-2000-2361. Reston: AIAA, 2000.
[14] Bird G A. Molecular gas dynamics and direct simulation of gas flow[M].London: Oxford University Press, 1994: 438-451.
[15] Huang L, Chen W F, Wu Q F. The studying of parallel algorithm for DSMC method with application to rarefied gas cylinder flow field[J]. Acta Aerodynamica Sinica, 2000, 18(4): 456-459. (in Chinese) 黄琳, 陈伟芳, 吴其芬.稀薄气体圆柱绕流的并行化DSMC方法研究[J].空气动力学学报, 2000, 18(4): 456-459.
[16] Wang X D, Wu Y Z, Xia J, et al. A paprallel algorithm of 3D unstructured DSMC method and its application[J]. Journal of Astronautics, 2007, 28(6): 1500-1505. (in Chinese) 王学德, 伍贻兆, 夏健, 等.三维非结构网格DSMC并行算法及应用研究[J].宇航学报, 2007, 28(6): 1500-1505.
[17] Fu Y, Hua R, Kang J C. Data migration dynamic load balance technology of DSMC parallel simulation[J]. Computer Engineering, 2004, 30(15): 66-68. (in Chinese) 傅游, 花嵘, 康继昌.DSMC并行仿真的数据迁移动态负载平衡技术[J].计算机工程, 2004, 30(15): 66-68.
[18] Wu Z N, Xu S S, Gao B, et al. Review of numerical computation of compressible flows with artificial interfaces[J]. Computers and Fluids, 2007, 36(10): 1657-1679.
[19] Padilla J F, Boyd I D. Assessment of rarefied hypersonic aerodynamics modeling and wind tunnel data, AIAA-2006-3390. Reston: AIAA, 2006. |