中国科学院机构知识库网格系统: 检索

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	Three-dimensional morphology and formation mechanism of tongue-shaped oblique detonation waves in elliptical flow channels 期刊论文 OAI收割 COMBUSTION AND FLAME, 2025, 卷号: 282, 页码: 14 作者: Niu, Shuzhen; Yang, Pengfei; Zhang, Zijian \| 收藏 \| 浏览/下载：14/0 \| 提交时间：2025/11/03 Hypersonic flow Oblique detonation wave Detonation combustion Flow channel
	Numerical Investigation of Freestream Composition Perturbations in a Scramjet Combustor 期刊论文 OAI收割 AIAA JOURNAL, 2025, 页码: 13 作者: Li XK(李新康); Yao W(姚卫); Yue LJ(岳连捷); Liu QL(刘起立) \| 收藏 \| 浏览/下载：11/0 \| 提交时间：2025/10/27 Hypersonic Shock Tunnel Scramjet Combustion Chambers Boundary Layer Separation Fuel Injection Combustor Design Fluid Mechanics Thrust Vectoring Numerical Simulation Vehicle Trajectories Partially Premixed Combustion
	Standing oblique detonation for hypersonic propulsion: A review 期刊论文 OAI收割 PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17 作者: Jiang ZL(姜宗林) \| 收藏 \| 浏览/下载：39/0 \| 提交时间：2024/02/26 Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion
	Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文 OAI收割 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14 作者: Yao, Wei; Liu, Hang; Xue, Lianjie; Xiao, Yabing; Yao W(姚卫) \| 收藏 \| 浏览/下载：59/0 \| 提交时间：2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet
	Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 OAI收割 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) \| 收藏 \| 浏览/下载：46/0 \| 提交时间：2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test
	Preliminary Investigation of Full Model of Two-Mode Scramjet 期刊论文 OAI收割 JOURNAL OF THERMAL SCIENCE, 2001, 卷号: 10, 期号: 2, 页码: 97,102 J.L. Le; Z.C. Zhang; H.C. Bai1; M.A. Goldfeld; R.V. Nestoulia; A.V. Starov2 收藏 \| 浏览/下载：31/0 \| 提交时间：2013/03/12 full engine hypersonic flow fuel inlet combustion wind tunnel experiment.
	Preliminary Investigation of Full Model of Two-Mode Scramjet 期刊论文 OAI收割 JOURNAL OF THERMAL SCIENCE, 2001, 卷号: 10, 期号: 2, 页码: 97,102 作者: J.L. Le; Z.C. Zhang; H.C. Bai1; M.A. Goldfeld; R.V. Nestoulia \| 收藏 \| 浏览/下载：35/0 \| 提交时间：2013/03/12 Full Engine Hypersonic Flow Fuel Inlet Combustion Wind Tunnel Experiment.
	Development of the facility for model scramjet testing 会议论文 OAI收割 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001 作者: Chang XY(张新宇); Chen LH(陈立红); Yu G(俞刚); Qian DX(钱大兴) 收藏 \| 浏览/下载：44/0 \| 提交时间：2017/06/01 Chinese Academy of Sciences Enthalpy flow Hypersonic propulsion test facility Performance tests Scramjet testing Supersonic combustion Total pressure Total temperatures