Thrust measurement of rotating detonation engine by sled test

Yuichi Kato, Kazuki Ishihara, Keita Gawahara, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki

研究成果: Conference contribution

7 被引用数 (Scopus)

抄録

Study of a Rotating Detonation Engine (RDE) has been carried out in many research institutions. The RDE has the advantage of high efficiency, simple structure and only once ignition. Toward the practical use for rocket engine, the evaluation of thrust efficiency and the knowledge of combustion under high acceleration or multiple degrees of freedom are essential. In this study, C2H4 + O2 mixture was used as propellant. A Slide mechanism for thrust measyrement was developed, and the mechanism reduced noise and exhausted burned gas. So, the thrust history was acquired and the thrust performance was assessed.

本文言語English
ホスト出版物のタイトル50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
出版社American Institute of Aeronautics and Astronautics Inc.
ISBN(電子版)9781624103032
DOI
出版ステータスPublished - 2014
イベント50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 - Cleveland, United States
継続期間: 2014 7月 282014 7月 30

出版物シリーズ

名前50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014

Other

Other50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
国/地域United States
CityCleveland
Period14/7/2814/7/30

ASJC Scopus subject areas

  • エネルギー工学および電力技術
  • 航空宇宙工学
  • 制御およびシステム工学
  • 電子工学および電気工学
  • 機械工学

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