Aerodynamic Characteristics and Flight Capability Prediction of the Small-scale Flight Experiment Vehicle Being Developed at Muroran Institute of Technology, Japan

摘要：

　　In order to research next-generation high-speed transportation technologies,Muroran Institute of Technology is developing a small-scale supersonic flight experiment vehicle(OWASHI the 2nd).Its aerodynamic characteristics are analyzed by wind tunnel tests and three-degree-and six-degree-of-freedom trajectory analysis predicts its flight capability.This paper describes the methods and results of the aerodynamic characterization and flight capability of OWASHI the 2nd.

关键词： Supersonic Experiment Vehicle Aerodynamic Characteristics Flight Capability Prediction Simulation

作者: Satoshi Kondo Yoshihiro Suzuki Muhammad Hanan Kazuhide Mizobata Ryojiro Minato Kazuyuki Higashino Nobuhiro Tanatsugu

作者单位: Graduate students,Muroran Institute of Technology,Hokkaido 050-8585,Japan Undergraduate student,Muroran Institute of Technology,Hokkaido 050-8585,Japan,presently Panasonic Ma Aerospace Plane Research Center,Muroran Institute of Technology,Hokkaido 050-8585,Japan

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: 1-7

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）