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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:7/0  |  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:30/0  |  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:28/0  |  提交时间:2024/02/26 Direct thermoelectric conversion Regenerative cooling Supersonic combustor Analytical model Genetic algorithm |
| Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model 期刊论文 COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 6 作者: Han X(韩信); Liu YF(刘云峰); Zhang, Zijian; Zhang WS(张文硕); Yuan CK(苑朝凯); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(1092Kb)  |  收藏  |  浏览/下载:70/4  |  提交时间:2023/11/28 |
| IDDES simulation of hydrogen-fueled supersonic combustion based on dynamic zone flamelet model 期刊论文 FUEL, 2023, 卷号: 347, 页码: 128502 作者: Zhang Z(张政); Yao W(姚卫); Wang Q(汪球); Zhao W(赵伟) Adobe PDF(17103Kb)  |  收藏  |  浏览/下载:148/1  |  提交时间:2023/06/15 Supersonic combustion Dynamic zone flamelet model Low-Reynolds correction Hydrogen Improved Delayed Detached Eddy Simulation |
| Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation 期刊论文 ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474 作者: Yuan CK(苑朝凯); Meng FZ(孟凡钊); Liu, Xu; Liu YF(刘云峰); Lian H(连欢); Liu, Yingzheng; Peng, Di Adobe PDF(3477Kb)  |  收藏  |  浏览/下载:43/1  |  提交时间:2023/07/17 Temperature-sensitive paint Heat flux Conjugate gradient method Air-breathing hypersonic vehicle Inverse heat conduction problem |
| 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:79/1  |  提交时间:2023/06/15 Hypervelocity combustion Thermal nonequilibrium Two-temperature model Numerical simulation |
| 动态飞行轨迹冲压发动机燃烧室性能与预测方法研究 学位论文 博士论文,北京: 中国科学院大学, 2023 作者: 周芮旭 Adobe PDF(9460Kb)  |  收藏  |  浏览/下载:96/8  |  提交时间:2023/06/28 动态飞行轨迹 超声速燃烧动态过程 燃烧室低维预测模型 |
| 自由斜爆轰起爆与驻定规律及其应用研究 学位论文 博士论文,北京: 中国科学院大学, 2023 作者: 张文硕 Adobe PDF(9967Kb)  |  收藏  |  浏览/下载:165/16  |  提交时间:2023/06/25 斜爆轰,起爆模式,时空关联,吸收光谱,冲压发动机 |
| 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:137/10  |  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 |