@article{oai:fukuyama-u.repo.nii.ac.jp:00008198,
 author = {真鍋, 圭司 and 中村, 弘明 and 西尾, 正富},
 journal = {福山大学工学部紀要},
 month = {Dec},
 note = {P(論文), Hypersonic flow field around the re-entry capsule is analyzed by Monte Carlo Simulation. The formulation for analyzing rarefied gas flow based on statistical theory is described. This method uses random number, and dynamics of molecular is simulated considering collision and reflection. The two dimensional capsule model is made by using Finite Element mesh, and hypersonic flow field of Mach 10 is calculated. The density and velocity field around the capsule model are calculated, and the shock wave is obtained as the density concentrated filed. This Monte Carlo method is considered to be effective for simulating hypersonic flow field, although some problems are remained.},
 pages = {273--276},
 title = {モンテカルロ法による極超音速流の解析},
 volume = {28},
 year = {2004}
}