Summary of CFD workshop using JAXA high-lift device wind tunnel model
| Autor: | Murayama, Mitsuhiro, Yamamoto, Kazuomi |
|---|---|
| Jazyk: | japonština |
| Rok vydání: | 2008 |
| Předmět: |
流体力
民間航空 high-lift device 計算流体力学 CFD Workshop computational fluid dynamics aerodynamic force 風洞試験 civil aviation passenger aircraft 風洞模型 CFDワークショップ 高揚力装置 航空機設計 低速風洞 boundary layer transition aircraft design 境界層遷移 grid generation wind tunnel model 比較 旅客機 comparison low speed wind tunnel 格子生成 wind tunnel test |
| Zdroj: | 宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :166-171 |
| ISSN: | 1349-113X |
| Popis: | A CFD (Computational Fluid Dynamics) workshop was held in the 44th Aircraft Symposium, October 2006, in order to evaluate domestic CFD technology for civil transport aircrafts in high-lift configurations. JAXA provided an experimental data for comparison obtained in the JAXA large low-speed wind tunnel using a half model equipped with high-lift devices, fuselage, nacelle-pylon, slat tracks and Flap Track Fairings (FTF). This paper briefly presents the experimental model, objectives and test cases of the CFD workshop, summary of comparison, and obtained knowledge and issues on CFD and wind tunnel testing for high-lift configuration. 資料番号: AA0063742027 レポート番号: JAXA-SP-07-016 |
| Databáze: | OpenAIRE |
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