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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  
On the robustness and accuracy of large-eddy simulation in predicting complex internal flow of a gas-turbine combustor 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 85120
作者:  Qiao Z(乔正);  Chen Y(陈与);  Wan, Kaidi;  Lv Y(吕钰)
Adobe PDF(7950Kb)  |  收藏  |  浏览/下载：29/0  |  提交时间：2023/09/05
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  
Numerical study of periodic flame flashback in a cavity-based scramjet combustor 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 45108
作者:  Guo SZ(郭升祖);  Zhang X(张旭);  Liu QL(刘起立);  Yue LJ(岳连捷)
Adobe PDF(5835Kb)  |  收藏  |  浏览/下载：61/1  |  提交时间：2023/06/15
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
作者:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Yu FY(于方游);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(582Kb)  |  收藏  |  浏览/下载：48/3  |  提交时间：2023/06/15
Scramjet Engines  Combustor Design  flame stabilization mode  transition  path dependence