Design of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed and Construction of its Prototype for Subsonic Flights
With the aims of creating and validating innovative fundamental technologies for high-speed atmospheric flights, a small scale supersonic experimental vehicle is designed as a flying test bed. Several aerodynamic configurations are proposed and analyzed by wind tunnel tests. A twin-engine configuration is selected as the baseline. Its flight capability is predicted by point mass analysis on the basis of aerodynamic characterization and propulsion performance estimation. In addition, a prototype vehicle with the equivalent configuration and dimension is designed and fabricated for verification of subsonic flight characteristics. Its first flight test is carried out and good flight capability is demonstrated.
Flying Test Bed Flight Experiment Supersonic Cranked Arrow Wing Jet Propulsion
Kazuhide MIZOBATA Ryojiro MINATO Katsuyoshi FUKIBA Kazuyuki HIGASHINO Nobuhiro TANATSUGU
Aerospace Plane Research Center, Muroran Institute of Technology 27-1, Mizumoto, Muroran, Hokkaido, 050-8585 Japan
国际会议
2011年亚太航空航天技术学术会议(APISAT 2011)
澳大利亚
英文
1-10
2011-02-28（万方平台首次上网日期，不代表论文的发表时间）