遷移領城流れのシミュレーション: DSMC法とNavier: Stokes数値解法

Material type: 文書・図像類

Author: 嶋田, 徹ほか

Publisher: 航空宇宙技術研究所

Publication date: 1991-12

Material Format: Digital

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Note (General)：: 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...

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Material Type: 文書・図像類
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
Author/Editor: 嶋田, 徹
和田, 安弘
古浦, 勝久
Shimada, Toru
Wada, Yasuhiro
Koura, Katsuhisa
Author Heading: 嶋田, 徹
和田, 安弘
古浦, 勝久
Shimada, Toru
Wada, Yasuhiro
Koura, Katsuhisa
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1991-12
Publication Date (W3CDTF): 1991-12
Alternative Title: Numerical Simulations of Hypersonic Rarefied Transition-Regime Flows -DSMC Method and Navier-Stokes Computation-
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-16
No. or year of volume/issue: 16
Volume: 16
Pages: 27-32
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): 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
Access Restrictions: 限定公開
Periodical Title (NCID): AN10097345
https://ci.nii.ac.jp/ncid/AN10097345
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ