遷音速全機形状まわりのパネル法計算と風洞試験の比較

Material type: 文書・図像類

Author: 海田, 武司ほか

Publisher: 航空宇宙技術研究所

Publication date: 1988-12

Material Format: Digital

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Note (General)：: The rapid progress of the computational aerodynamics enables us to analyze airflow with viscous calculation instead of with invisid one. In two-dimens...

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Material Type: 文書・図像類
Title: 遷音速全機形状まわりのパネル法計算と風洞試験の比較
Author/Editor: 海田, 武司
宮川, 淳一
柳沢, 三憲
天野, 完一
Kaiden, Takeshi
Miyakawa, Jun-ichi
Yanagisawa, Mitsunori
Amano, Kan-ichi
Author Heading: 海田, 武司
宮川, 淳一
柳沢, 三憲
天野, 完一
Kaiden, Takeshi
Miyakawa, Jun-ichi
Yanagisawa, Mitsunori
Amano, Kan-ichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1988-12
Publication Date (W3CDTF): 1988-12
Alternative Title: Comparison with Computation Using Panel Method and Wind Tunnel Test Around Transonic Complete Aircraft
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-9
No. or year of volume/issue: 9
Volume: 9
Pages: 141-150
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): The rapid progress of the computational aerodynamics enables us to analyze airflow with viscous calculation instead of with invisid one. In two-dimensional application, we have already validated its effectiveness in comparison with wind tunnel testing and put it into practical stage. In three-dimensional application, the wing-body configulation has been also done. This paper presents a validative discussion of the panel method toward the analysis about the complete aircraft, including the calculation of the sting interference, which is indispensable to wind tunnel testing. The results indicate that the panel method is valid in the subsonic region and that the sting makes up wash flow.
資料番号: NALSP0009021
レポート番号: NAL SP-9
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