ナビェ・ストークス方程式による尾翼回りの流れの解析

Material type: 文書・図像類

Author: 越岡, 康弘ほか

Publisher: 航空宇宙技術研究所

Publication date: 1987-11

Material Format: Digital

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Note (General)：: Flow field simulations over transonic transport aircraft empennage were carried out based on three-dimensional Navier-Stokes equations. The computatio...

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Material Type: 文書・図像類
Title: ナビェ・ストークス方程式による尾翼回りの流れの解析
Author/Editor: 越岡, 康弘
加茂, 圭介
天野, 完一
Koshioka, Yasuhiro
Kamo, Keisuke
Amano, Kan-ichi
Author Heading: 越岡, 康弘
加茂, 圭介
天野, 完一
Koshioka, Yasuhiro
Kamo, Keisuke
Amano, Kan-ichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1987-11
Publication Date (W3CDTF): 1987-11
Alternative Title: Navier-Stokes Analysis of Transonic Transport Aircraft Empennage
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: 49-54
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): Flow field simulations over transonic transport aircraft empennage were carried out based on three-dimensional Navier-Stokes equations. The computations were done for the flow fields of various Mach numbers and angles of attack to investigate the variation of the lift curve slope with Mach number at low angle of attack, and the variation of the lift coefficient with angle of attack at low Mach number. The values of lift curve slope obtained by the computations show good agreement with those by experiments. While the difference between computations and experiments looks a little large about lift coefficient versus angle of attack.
資料番号: NALSP0008007
レポート番号: NAL SP-8
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