@techreport{oai:jaxa.repo.nii.ac.jp:00043501,
 author = {嶋田, 徹 and 和田, 安弘 and 古浦, 勝久 and Shimada, Toru and Wada, Yasuhiro and Koura, Katsuhisa},
 month = {Dec},
 note = {Numerical solutions of the direct-simulation Monte Carlo (DSMC) method and the Navier-Stokes equation with a no-slip or a slip wall boundary condition are obtained for hypersonic rarefied monatomic gas flows in the transition regime (kn=0.1 - 0.001) around a finite-length parallel flat plate and a circular cylinder. A comparison among these numerical solutions indicates that the DSMC method is well applied to a fully continuum flow regime and the Navier-Stokes equation is applicable to the transition flow regime by the use of the slip wall boundary condition., 資料番号: NALSP0016005, レポート番号: NAL SP-16},
 title = {遷移領城流れのシミュレーション: DSMC法とNavier: Stokes数値解法},
 year = {1991}
}