1. Summary of CFD workshop using JAXA high-lift device wind tunnel model
- Author
-
Murayama, Mitsuhiro and Yamamoto, Kazuomi
- Subjects
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 - Abstract
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
- Published
- 2008