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| Study on the propulsive performance of oblique detonation engine 期刊论文
ENERGY, 2024, 卷号: 292, 页码: 11
作者: Liu YF(刘云峰) ; Han, Xin; Zhang, Zijian
  收藏 | 浏览/下载：1/0 | 提交时间：2024/04/15
Oblique detonation engine ODE Propulsive performance Specific impulse |
| Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
作者: Liu H(刘杭); Yao W(姚卫); Zhang X(张旭); Zhang XY(张晓源); Liu, Jianwen; Yue LJ(岳连捷); Sun QH(孙泉华)
收藏 | 浏览/下载：26/0 | 提交时间：2024/03/11
Scramjet Dynamic Zone Flamelet Model High Enthalpy Shock Tunnel Combustors Improved Delayed Detached Eddy Simulation Vibrational Energy nonequilibrium heating cooling effects thermal nonequilibrium chemical nonequilibrium hydrogen |
| Study on heat transfer coupling mechanism of direct thermoelectric conversion with regenerative cooling for supersonic combustor applications 期刊论文
APPLIED THERMAL ENGINEERING, 2024, 卷号: 238, 页码: 15
作者: Gao EK(高尔康); Zhong FQ(仲峰泉)
收藏 | 浏览/下载：24/0 | 提交时间：2024/02/26
Direct thermoelectric conversion Regenerative cooling Supersonic combustor Analytical model Genetic algorithm |
| Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions 期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 208, 页码: 281-295
作者: Ao Y(敖彧); Wu K(吴坤); Lu, Hongbo; Ji, Feng; Fan XJ(范学军)
 Adobe PDF(11339Kb) | 收藏 | 浏览/下载：75/0 | 提交时间：2023/06/15
Hypervelocity combustion Thermal nonequilibrium Two-temperature model Numerical simulation |
| 高马赫数超燃冲压发动机燃烧室再生冷却特性研究 学位论文
博士论文，北京: 中国科学院大学, 2023
作者: 徐雪睿
Adobe PDF(12526Kb) | 收藏 | 浏览/下载：125/10 | 提交时间：2023/06/27
高马赫数 超燃冲压发动机 理论分析 解离效率 再生冷却 组合式冷却方法 超临界CO2布雷顿循环 |
| 再生冷却通道微结构强化传热与流动机理研究 学位论文
博士论文，北京: 中国科学院大学, 2022
作者: 李冼
Adobe PDF(65313Kb) | 收藏 | 浏览/下载：382/8 | 提交时间：2023/01/11
再生冷却 航空煤油 凹陷窝 微肋 强化传热 |
| Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
作者: Liu, Mingjiang; Sun, Mingbo; Zhao, Guoyan; Meng Y(孟宇); Huang, Yuhui; Ma, Guangwei; Wang, Hongbo
Adobe PDF(3841Kb) | 收藏 | 浏览/下载：96/21 | 提交时间：2022/12/20
Tandem-cavity Scramjet combustor Combustion mode Thrust performance |
| Experimental study of hysteresis and catastrophe in a cavity-based scramjet combustor 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 10, 页码: 118-133
作者: Zhang X(张旭); Zhang QF(张启帆); Wu ZJ(吴振杰); Yue LJ(岳连捷); Gao ZB(高占彪); Luo WH(罗苇航); Chen H(陈昊)
Adobe PDF(4834Kb) | 收藏 | 浏览/下载：25/1 | 提交时间：2023/07/17
Catastrophe Cavity-based scramjet Flame stabilization Flame/shock interaction Hysteresis |
| Comprehensive Analyses on the Influential Factors in Supersonic Combustion Simulation Using Dynamic Adaptive Chemistry Method 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2022, 页码: 29
作者: Wu K(吴坤); Contino, Francesco; Fan XJ(范学军)
Adobe PDF(14452Kb) | 收藏 | 浏览/下载：222/21 | 提交时间：2022/09/27
Dynamic adaptive chemistry mechanism reduction method error threshold search initiating species High-fidelity numerical simulation |
| Effect of helical fins on the combustion performance in a micro-step combustor 期刊论文
FUEL, 2022, 卷号: 319, 页码: 13
作者: Zhang Z(张政); Shen WBY; Yao W(姚卫); Wang Q(汪球); Zhao W(赵伟)
Adobe PDF(11881Kb) | 收藏 | 浏览/下载：234/27 | 提交时间：2022/05/17
Micro-combustion Helical fin Combustion performance Conjugate heat transfer Mixing |
