NACA0012翼まわりの遷音速流に関する予備研究

Material type: 文書・図像類

Author: サキャ, アンディエカほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-11

Material Format: Digital

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Note (General)：: A typical transonic flow at M infinity =0.80 and Re=1 by 106 is numerically simulated by using the Yee-Harten TVD Scheme of Euler Backward Implicit me...

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Material Type: 文書・図像類
Title: NACA0012翼まわりの遷音速流に関する予備研究
Author/Editor: サキャ, アンディエカ
中村, 佳朗
保原, 充
Sakya, Andi E.
Nakamura, Yoshiaki
Yasuhara, Michiru
Author Heading: サキャ, アンディエカ
中村, 佳朗
保原, 充
Sakya, Andi E.
Nakamura, Yoshiaki
Yasuhara, Michiru
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-11
Publication Date (W3CDTF): 1989-11
Alternative Title: A Preliminary Study of Transonic Flow around NACA0012
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10
No. or year of volume/issue: 10
Volume: 10
Pages: 255-264
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): A typical transonic flow at M infinity =0.80 and Re=1 by 106 is numerically simulated by using the Yee-Harten TVD Scheme of Euler Backward Implicit method. This study treats unsteady, inviscid or viscous compressible flows. In the viscous flow case, two turbulence models are applied: Baldwin-Lomax model (BLM) and Stock-Haase model (SHM). Comparison with the experimental data shows a good agreement.
資料番号: NALSP0010043
レポート番号: NAL SP-10
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43372&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43372&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