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Bibliographic Record
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- Material Type
- 規格・テクニカルリポート類
- Author/Editor
- 宮川, 淳一高梨, 進藤井, 孝蔵天野, 完一Miyakawa, Jun-ichiTakanashi, SusumuFujii, KozoAmano, Kan-ichi
- Publication, Distribution, etc.
- Publication Date
- 1986-12
- Publication Date (W3CDTF)
- 1986-12
- Alternative Title
- Numerical Simulation of Transonic Aircraft in Comparison to Wind Tunnel Test
- 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
- 299-314
- ISSN (Periodical Title)
- ISSN : 0289-260X
- Text Language Code
- jpn
- Target Audience
- 一般
- Note (General)
- 出版タイプ： NAComputational aerodynamics has evolved to the point where it has become a practical design tool comparable to wind tunnel tesing and has played an important role in actual aircraft design stages. The Navier-Stokes code, however, is still restricted to two-dimensional applications, which have been repeatedly validated in this symposium. The three-dimensional application, which is a real challenge for the Navier-Stokes code, is discussed in this paper for the first time, If this three-dimensional application could be perfected, it would be a big step toward the final target of complete aircraft analysis by numerical simulation.資料番号: NALSP0007036レポート番号: NAL SP-7
- Periodical Title (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）
- 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