Aerospace Plane Research Center, Muroran Institute of Technology
Aerospace Plane Research Center, Muroran Institute of Technology
Aerospace Plane Research Center, Muroran Institute of Technology
Aerospace Plane Research Center, Muroran Institute of Technology
Aerospace Plane Research Center, Muroran Institute of Technology
Aerospace Plane Research Center, Muroran Institute of Technology
出版者
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
雑誌名
平成24年度宇宙輸送シンポジウム: 講演集録
雑誌名(英)
Proceedings of Space Transportation Symposium: FY2012
Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
With the aims of creating and validating innovative fundamental technologies for high-speed atmospheric flights, a small-scale supersonic experimental vehicle is being developed as a flying test bed. The configuration M2006 with a cranked-arrow main wing and twin engines was designed and its aerodynamic characteristics were verified through wind-tunnel and flight tests. A new configuration M2011 with a main wing and tails of similar shapes and a single GG-ATR engine was proposed. Intensive wind-tunnel tests were carried out in transonic and supersonic regimes. It was found that the overall drag coefficient increases as the intake passage is throttled and that the airflow through the intake seems to be squeezed by the development of the boundary layer. In addition, the tail steering box located at the vertical tail root has little influence on overall drag.
内容記述
形態: カラー図版あり
形態: PDF
内容記述（英）
Physical characteristics: Original contains color illustrations
Physical characteristics: PDF
小型超音速飛行実験機の風洞試験に基づく機体抗力検討
61856059.pdf
(2.94MB)
