ダイナミック・ストールの数値解析

Material type: 文書・図像類

Author: 信太, 良文ほか

Publisher: 航空宇宙技術研究所

Publication date: 1986-12

Material Format: Digital

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Note (General)：: The flow field around an oscillating NACA0012 airfoil in pitch at 0.25 chord is analyzed by solving the two-dimensional compressible Navier-Stokes equ...

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Material Type: 文書・図像類
Title: ダイナミック・ストールの数値解析
Author/Editor: 信太, 良文
桑原, 邦郎
Shida, Yoshifumi
Kawahara, Kunio
Author Heading: 信太, 良文
桑原, 邦郎
Shida, Yoshifumi
Kawahara, Kunio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1986-12
Publication Date (W3CDTF): 1986-12
Alternative Title: Computation of Dynamic Stall of NACA0012 Airfoil by Block Pentadiagonal Matrix Scheme
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-7
No. or year of volume/issue: 7
Volume: 7
Pages: 13-24
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): The flow field around an oscillating NACA0012 airfoil in pitch at 0.25 chord is analyzed by solving the two-dimensional compressible Navier-Stokes equations. A block pentadiagonal matrix scheme based on the approximate factorization method is adopted. Two meshes, 161 by 40 and 213 by 80, are used. With the coarse mesh, lift stall is cap-tured. With the fine mesh, not only lift stall but also the restoration process of the lift coefficient in the downstroke is captured.
資料番号: NALSP0007002
レポート番号: NAL SP-7
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43218&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43218&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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）
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