机构

• 力学研究所 [7]
• 工程热物理研究所 [2]

采集方式

• OAI收割 [9]

内容类型

• 期刊论文 [7]
• 会议论文 [2]

发表日期

• 2023 [1]
• 2021 [2]
• 2016 [1]
• 2013 [1]
• 2009 [1]
• 2006 [1]
• 更多

学科主题

• Engineerin... [1]
• 流体力学::内流 [1]

筛选

浏览/检索结果: 共9条，第1-9条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 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：12/0  |  提交时间：2024/02/26 Standing oblique detonation  Scramjet engine  Oblique detonation engine  Shock wave  Supersonic combustion  Hypersonic ramjet propulsion   Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文  OAI收割 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788 作者:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin   |  收藏  |  浏览/下载：35/0  |  提交时间：2022/10/25 Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine   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：25/0  |  提交时间：2021/05/17 Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test   Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文  OAI收割 ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82 作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇) 收藏  |  浏览/下载：23/0  |  提交时间：2016/09/14 Dual-mode scramjet  Engine performance  Thrust  Optimization  Heat release distribution  Simulated annealing algorithm   Theoretical analysis of effects of boundary layer bleed on scramjet thrust 期刊论文  OAI收割 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961 作者:  Yue LJ(岳连捷);  Xu XK(徐显坤);  Zhang XY(张新宇) 收藏  |  浏览/下载：21/0  |  提交时间：2013/10/23 scramjet  boundary layer bleed  theoretical analysis  engine thrust   Performance of the fuel injector in supersonic combustor 会议论文  OAI收割 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009 作者:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙) 收藏  |  浏览/下载：21/0  |  提交时间：2017/07/14 Concentration profiles  Engine design  Fuel injectors  Fuel-air mixing  Gas sampling  Ramp injector  Scramjet combustors  Scramjet test  Supersonic combustors   Experimental investigation of cavity-based scramjet model 会议论文  OAI收割 14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006 作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY) 收藏  |  浏览/下载：20/0  |  提交时间：2017/06/01 Kerosene fuel  Mass flow rate  Scramjet engine   The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 371,380 Mohammad Ali; S. Ahmed; A.K.M. Sadrul Islam 收藏  |  浏览/下载：14/0  |  提交时间：2013/03/12 scramjet engine  TVD scheme  finite width of inlet  supersonic mixing  parallel air stream  flame holding.   The Effect of Injection Angle on Mixing and Flame Holding in Supersonic Combustor 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2002, 卷号: 11, 期号: 1, 页码: 80,91 Shakil Ahmed; Mohammad Ali; A. K. M. Sadrul Islam 收藏  |  浏览/下载：14/0  |  提交时间：2013/03/12 scramjet engine  TVD scheme  backward-facing step  supersonic mixing  supersonic stream  flame holding.