Development of Aeroelastic Simulation Code Using Unstructured CFD Solver

摘要：

　　This paper describes that a new aeroelastic simulation code based on the unstructured CFD solver is developed.Computations are performed for AGARD 445.6 wing model.The Flutter boundary predicted by the developed code are presented and compared with the experimental data.

关键词： Aeroelastic Simulation CFD solver

作者: Hitoshi Arizono Hamid Reza Kheirandish

作者单位: Japan Aerospace Exploration Agency,6-13-1 Osawa Mitaka Tokyo,181-0065,Japan Research Center of Computational Mechanics,Inc.,Togoshi N1-Bldg.,1-7-1 Togoshi Shinagawa Tokyo,142-0

会议类型: 国际会议

会议名称: 2014 Asia-Pacific International Symposium on Aerospace Technology(2014亚太航空航天技术学术会议)

会议地点: 上海

会议语种:英文

页码: 1-4

在线出版日期: 2014-09-24（万方平台首次上网日期，不代表论文的发表时间）