3次元N-S解析コードのタービン翼列設計への応用

Material type: 文書・図像類

Author: 菊地, 一雄ほか

Publisher: 航空宇宙技術研究所

Publication date: 1990-11

Material Format: Digital

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Note (General)：: This paper presents an application of the 3-D Navier-Stokes computations in designing a turbine vane cascade. The accurate prediction of the cascade f...

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Material Type: 文書・図像類
Title: 3次元N-S解析コードのタービン翼列設計への応用
Author/Editor: 菊地, 一雄
野崎, 理
田村, 敦宏
松永, 康二
竹内, 久雄
真家, 孝
山脇, るり子
Kikuchi, Kazuo
Nozaki, Osamu
Tamura, Atsuhiro
Matsunaga, Koji
Takeuchi, Hisao
Maya, Takasi
Yamawaki, Ruriko
Author Heading: 菊地, 一雄
野崎, 理
田村, 敦宏
松永, 康二
竹内, 久雄
真家, 孝
山脇, るり子
Kikuchi, Kazuo
Nozaki, Osamu
Tamura, Atsuhiro
Matsunaga, Koji
Takeuchi, Hisao
Maya, Takasi
Yamawaki, Ruriko
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1990-11
Publication Date (W3CDTF): 1990-11
Alternative Title: Application of 3-D Navier-Stokes Computation to Turbine Vane Design
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-14
No. or year of volume/issue: 14
Volume: 14
Pages: 249-255
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): This paper presents an application of the 3-D Navier-Stokes computations in designing a turbine vane cascade. The accurate prediction of the cascade flow characteristics such as total pressure loss and outlet flow angle is important for aerodynamic engineers to evaluate the performance of airfoil contour shapes. Here a curvilinear leaned stator vane, adopted to supress the secondary flow and reduce the losses, is studied in detail. The advanced design based on the 3-D Navier-Stokes computations succeeded to reduce the losses greatly showing the capability of the code as a design tool.
資料番号: NALSP0014040
レポート番号: NAL SP-14
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