側壁付きONERA-M6翼まわりの非定常計算

Material type: 文書・図像類

Author: 桜木, 卓也ほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-11

Material Format: Digital

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Note (General)：: The major portion of the flow field at high Reynolds number will be unsteady, so turbulent eddy viscosity models are used in simulating such high Reyn...

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Material Type: 文書・図像類
Title: 側壁付きONERA-M6翼まわりの非定常計算
Author/Editor: 桜木, 卓也
加茂, 圭介
Sakuragi, Takuya
Kamo, Keisuke
Author Heading: 桜木, 卓也
加茂, 圭介
Sakuragi, Takuya
Kamo, Keisuke
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-11
Publication Date (W3CDTF): 1989-11
Alternative Title: Unsteady Calculation of the Transonic Flow Over the ONERA-M6 Wing with a Side Wall
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: 33-38
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): The major portion of the flow field at high Reynolds number will be unsteady, so turbulent eddy viscosity models are used in simulating such high Reynolds number flow. The steady flow fields obtained by using turbulent eddy viscosity model is expected to be the time-averaged solutions. In this study, we investigated the unsteady solution of the flow over the wing with a side wall. For this purpose, we calculated the time-average of the unsteady flow field without using any turbulent eddy viscosity models. As the number of grid points gets large, the CP-curves of the time-average will become close to the results of the experiment.
資料番号: NALSP0010006
レポート番号: NAL SP-10
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43335&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43335&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