70. 参考文献 (References)


1) Bird, G. A.: Molecular Gas Dynamics, Clarendon, Oxford, 1976.

2) Bird, G. A.: Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Clarendon, Oxford, 1994.

3) 日本機械学会編: 計算力学ハンドブック第Ⅲ巻 (4.1 DSMC法の基礎),日本機械学会,2009,pp. 130-149.[特記] 宇佐美によるFORTRANソースコード(Bird method)閲覧可.[Special note] Usami’s FORTRAN source code (Bird method) can be viewed.

4) Usami, M. and Nakayama, T.: Intermolecular Collision Scheme of DSMC Taking Molecular Locations within a Cell into Account, Rarefied Gas Dynamics 23, AIP Conference Proceedings, 663 (2003), pp. 374-381.

5) Usami, M. and Mizuguchi, K.: DSMC Calculation of Vortex Shedding behind a Flat Plate with a New Intermolecular Collision Scheme, Rarefied Gas Dynamics 24, AIP Conference Proceedings, 762 (2005), pp. 686-691.

6) 宇佐美勝: 衝突計算を改良したDSMC法の圧縮性流体への適用,ながれ,26, 4 (2007),pp. 273-282.

7) Sun, Q., Liu, H. and Fan, J.: Development of a Cell Size Relaxed Scheme for the Direct Simulation Monte Carlo Method, Rarefied Gas Dynamics 26, AIP Conference Proceedings, 1084 (2009), pp. 311-316.

8) Pareschi, L. and Trazzi, S.: Numerical Solutions of the Boltzmann Equation by Time Relaxed Monte Carlo (TRMC) Methods, Int. J. Numerical Methods in Fluids, 48, 9 (2005), pp. 947-983.

9) 宇佐美勝,久保 貴,北山隼平: 一次元垂直衝撃波のDSMC解析における分子間衝突法に関する研究,航空宇宙技術,14 (2015),pp. 123-130. [特記] 宇佐美によるFORTRANソースコード(一次元 U_system)をその電子付録で閲覧可.
Usami, M., Kubo, T. and Kitayama, J.: DSMC Analysis of One-dimensional Normal Shock Wave (Study on Intermolecular Collision Scheme), Kōkū Uchū Gijutsu (Japanese paper of the Japan Society of Aeronautics and Astronautics), Vol.14 (2015),pp. 123-130. [Special note] Usami’s FORTRAN source code (one-dimensional U_system) can be viewed on its appendix.

10) 宇佐美勝,古川裕之:不足膨張噴流の DSMC 計算,航空宇宙技術,15 (2016),pp. 117-125. [特記] DSMC法のPCによる並列計算技法についても記述してある.
Usami, M. and Furukawa, H.: DSMC Calculation on Underexpanded Jets, Kōkū Uchū Gijutsu (Japanese paper of the Japan Society of Aeronautics and Astronautics), Vol.15 (2016),pp. 117-125. [Special note] A parallel calculation technique for the DSMC method using a PC is also described.

11) 宇佐美勝:一次元垂直衝撃波のDSMC解析における分子間衝突法に関する研究(第2報 セル内分子数と平均自由行程),航空宇宙技術,16 (2017),pp. 37-44.
Usami, M.: Study on Intermolecular Collision Scheme for DSMC Analysis of One-dimensional Normal Shock Wave (Second Report: Number of Molecules per Cell and Mean Free Path), Kōkū Uchū Gijutsu (Japanese paper of the Japan Society of Aeronautics and Astronautics), Vol.16 (2017),pp. 37-44.

12) Bird, G. A.: Direct Simulation of High-Vorticity Gas Flows, Phys. Fluids, 30-2 (1987), 364-366.

13) Bird, G. A.: Monte-Carlo Simulation in an Engineering Context, Progress in Astronautics and Aeronautics, 74 (1981), 239-255, AIAA.

14) Bird, G. A.: Perception of Numerical Methods in Rarefied Gasdynamics, Progress in Astronautics and Aeronautics, 118 (1989), 211-226, AIAA.

15) 宇佐美勝,手島光司:DSMC 法による超音速希薄自由噴流の分子シミュレーション,機論,64-620, B (1998), 1112-1119.

16) Usami, M., Fujimoto, T. and Kato, S.: Monte Carlo Simulation on Mass Flow Reduction due to Roughness of a Slit Surface, Progress in Astronautics and Aeronautics, 116 (1989), 283-297, AIAA.

17) Koura, K. and Matsumoto, H.: Variable Soft Sphere Molecular Model for Inverse-Power-Law or Lennard-Jones Potential, Phys. Fluids A, 3-10 (1991), 2459-2465.

18) Hermina, W. L.: Monte Carlo Simulation of High Altitude Rocket Plumes with Nonequilibrium Molecular Energy Exchange, Proc. AIAA/ASME 4th Joint Thermophys. Heat Transf. Conf., (1986), AIAA-86-1318.

19) Koura, K.: Null Collision Monte Carlo Method: Gas Mixtures with Internal Degrees of Freedom and Chemical Reactions, Progress in Astronautics and Aeronautics, 117 (1989), 25-39, AIAA.

20) Nanbu, K.: Theoretical Basis of the Direct Simulation Monte Carlo Method, Proc. 15th Int. Symp. Rarefied Gas Dynamics, 1 (1986), 369-383.

21) Borgnakke, C. and Larsen, P. S.: Statistical Collision Model for Monte Carlo Simulation of Polyatomic Gas Mixture, Computational Physics, 18 (1975), 405-420.