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規格・テクニカルリポート類

反変速度成分の圧縮性ナビエ・ストークス方程式の陰的時間進行法

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反変速度成分の圧縮性ナビエ・ストークス方程式の陰的時間進行法

Material type
規格・テクニカルリポート類
Author
大宮司, 久明ほか
Publisher
航空宇宙技術研究所
Publication date
1988-12
Material Format
Digital
Capacity, size, etc.
-
NDC
-
View Details

Notes on use

Note (General):

The implicit time-marching finite-difference method for solving the three-dimensional compressible Euler equations developed by the authors is extende...

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Digital

Material Type
規格・テクニカルリポート類
Author/Editor
大宮司, 久明
山本, 悟
Daiguji, Hisaaki
Yamamoto, Satoru
Publication, Distribution, etc.
Publication Date
1988-12
Publication Date (W3CDTF)
1988-12
Alternative Title
An Implicit Time-Marching Method for the Three-Dimensional Navier-Stokes Equations of Contravariant Velocity Components
Periodical title
航空宇宙技術研究所特別資料
No. or year of volume/issue
9
Volume
9
Pages
77-84
ISSN (Periodical Title)
ISSN : 0289-260X
Text Language Code
jpn
Target Audience
一般
Note (General)
The implicit time-marching finite-difference method for solving the three-dimensional compressible Euler equations developed by the authors is extended to the Navier-Stokes equations. The distinctive features of this method are to make use of the momentum equations of contravariant velocities instead of the physical velocities, and to be able to treat the periodic boundary condition for the 3-D impeller flow easily. These equations can be solved by using the same techniques as the Euler equations, such as the delta-form approximate factorization, diagonalization and upstreaming. In addition to them, a simplified TVD scheme by the authors is applied to the present method in order to capture strong shock waves clearly. Finally, the computed results of the 3-D flow through a transonic compressor rotor with tip clearance are shown.
資料番号: NALSP0009012
レポート番号: NAL SP-9
Access Restrictions
インターネット公開
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)
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