非定常圧縮性ナビエ・ストークス方程式に対する高精度陰解法

Material type: 文書・図像類

Author: 松野, 謙一ほか

Publisher: 航空宇宙技術研究所

Publication date: 1988-12

Material Format: Digital

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Note (General)：: In this paper a time accurate scheme for unsteady Navier-Stokes equations is presented. This scheme employs, as unknowns, quantities of order of squar...

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Material Type: 文書・図像類
Title: 非定常圧縮性ナビエ・ストークス方程式に対する高精度陰解法
Author/Editor: 松野, 謙一
Matsuno, Ken-ichi
Author Heading: 松野, 謙一
Matsuno, Ken-ichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1988-12
Publication Date (W3CDTF): 1988-12
Alternative Title: An Implicit Scheme for Unsteady Compressible Navier-Stokes Equations
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-9
No. or year of volume/issue: 9
Volume: 9
Pages: 93-96
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): In this paper a time accurate scheme for unsteady Navier-Stokes equations is presented. This scheme employs, as unknowns, quantities of order of square of time spacing, thus making a "delta2-form", of which the right hand side is a numerical approximation of unsteady governing equations. This argorithm makes a scheme especially suitable for time accurate simulations A shock tube flow is calculated as an example. The flow is assumed laminar, and shock wave-boundary layer interaction is simulated.
資料番号: NALSP0009014
レポート番号: NAL SP-9
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