A Review of principles and key techniques for Supersonic Pulsed Detonation Ramjet Engine (SPDRE)

摘要：

Supersonic Pulsed Detonation Ramjet Engine (SPDRE) is a novel and promising alternative for idea propulsion systems for future supersonic aircrafts, which utilizes the internal instabilities of detonation waves caused by the alternations of mixing ratios, and obtains thrust by means of organizing pulsed-oscillating detonation waves in supersonic reactive flows. The conception and basic principles of SPDRE are introduced in the present work. A detailed review of the key techniques is addressed, as well as the research progress and status. Suggestions on future aspects and emphases for the fundamental studies of SPDRE are put forward.

作者: Hui Qin Zhiyong Lin Weidong Liu Zhenguo Wang

作者单位: Institute of Aerospace & Material Engineering,National University of Defense Technology,Changsha,410073,China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1090-1094

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）