Jump to main content
規格・テクニカルリポート類

指数表現を用いたk-ε方程式による乱流場の数値シミュレーション

Icons representing 規格・テクニカルリポート類

指数表現を用いたk-ε方程式による乱流場の数値シミュレーション

Material type
規格・テクニカルリポート類
Author
日夏, 宗彦ほか
Publisher
航空宇宙技術研究所
Publication date
1987-11
Material Format
Digital
Capacity, size, etc.
-
NDC
-
View Details

Notes on use

Note (General):

出版タイプ: NAThis paper presents a numerical simulation of a turbulent flow around a wing section by use of k-epsilon turbulence model. In order to assure...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

  • JAXA Repository

    Digital
    You can check the holdings of institutions and databases with which Institutional Repositories DataBase(IRDB)(Institutional Repository) is linked at the site of Institutional Repositories DataBase(IRDB)(Institutional Repository).

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type
規格・テクニカルリポート類
Author/Editor
日夏, 宗彦
児玉, 良明
Hinatsu, Munehiko
Kodama, Yoshiaki
Publication, Distribution, etc.
Publication Date
1987-11
Publication Date (W3CDTF)
1987-11
Alternative Title
Numerical Simulation of Turbulent Flow Using the Exponential Expression of k-epsilon Equation
Periodical title
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-8
No. or year of volume/issue
8
Volume
8
Pages
225-232
ISSN (Periodical Title)
ISSN : 0289-260X
Text Language Code
jpn
Target Audience
一般
Note (General)
出版タイプ: NA
This paper presents a numerical simulation of a turbulent flow around a wing section by use of k-epsilon turbulence model. In order to assure the positiveness of k and epsilon, the exponential expression of k-epsilon is used. IAF method is adopted as a computational scheme. A new treatment for the boundary condition on the wing surface is devised. A turbulent flow around NACA0012 wing section with 5-deg. angle of attack at Re=106 is simulated.
資料番号: NALSP0008032
レポート番号: NAL SP-8
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