Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 11 Help

Filters                
Selected(0)Clear Items/Page:    Sort:
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
Authors:  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)  |  Favorite  |  View/Download：32/2  |  Submit date：2023/07/17
Catastrophe  Cavity-based scramjet  Flame stabilization  Flame/shock interaction  Hysteresis  
Experimental investigation of combustion-induced starting hysteresis in the scramjet 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 9, 页码: 96103
Authors:  Zhang QF(张启帆);  Chen H(陈昊);  Wu ZJ(吴振杰);  Gao ZB(高占彪);  Luo WH(罗苇航);  Gu HB(顾洪斌);  Yue LJ(岳连捷)
Adobe PDF(2852Kb)  |  Favorite  |  View/Download：162/50  |  Submit date：2022/10/23
Switching between symmetric and asymmetric separation-induced shock reflections in an oscillatory duct flow 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 7, 页码: 71703
Authors:  Chen H(陈昊);  Zhang QF(张启帆);  Luo WH(罗苇航);  Yue LJ(岳连捷)
Adobe PDF(2855Kb)  |  Favorite  |  View/Download：124/35  |  Submit date：2022/10/23
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Zhang X(张旭);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(3049Kb)  |  Favorite  |  View/Download：165/24  |  Submit date：2022/07/18
高马赫数燃烧强化的激波风洞试验研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413
Authors:  张旭;  张启帆;  岳连捷;  孟东东;  罗苇航;  于江鹏;  张晓源;  李进平;  陈宏;  李飞
Adobe PDF(3069Kb)  |  Favorite  |  View/Download：256/48  |  Submit date：2022/08/11
高马赫数  超声速燃烧  燃烧强化  小支板  JF-24激波风洞  
基于动态分区概念的高超声速燃烧大涡模拟 期刊论文
力学学报, 2022, 卷号: 54, 期号: 04, 页码: 954-974
Authors:  姚卫;  刘杭;  张政;  肖雅彬;  岳连捷
Adobe PDF(1875Kb)  |  Favorite  |  View/Download：300/71  |  Submit date：2022/06/10
高超声速燃烧  动态分区火焰面  分区自适应化学  分区并行自适应建表  改进延迟分离涡模拟  
斜激波串非对称特性研究 期刊论文
推进技术, 2022, 卷号: 43, 期号: 04, 页码: 101-108
Authors:  黄庭隆;  贺理浩;  岳连捷
Adobe PDF(1632Kb)  |  Favorite  |  View/Download：173/42  |  Submit date：2022/06/10
隔离段  斜激波串  非对称性  建模分析  数值仿真  
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
Authors:  Dai, Chunliang;  Sun, Bo;  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(13791Kb)  |  Favorite  |  View/Download：176/40  |  Submit date：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
On the Reynolds-Number Sensitivity of Inlet Flow at Mach Numbers Beyond 7 期刊论文
AIAA JOURNAL, 2022, 卷号: 60, 期号: 3, 页码: 1978-1982
Authors:  Chen H(陈昊);  Wang ZR;  Zhang QF(张启帆);  Zhang XY(张晓源);  Yue LJ(岳连捷)
Adobe PDF(625Kb)  |  Favorite  |  View/Download：123/30  |  Submit date：2022/10/25
高马赫数超燃冲压发动机技术研究进展 期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:  岳连捷;  张旭;  张启帆;  陈科挺;  李进平;  陈昊;  姚卫;  仲峰泉;  李飞;  王春;  陈宏
Adobe PDF(2622Kb)  |  Favorite  |  View/Download：560/104  |  Submit date：2022/03/16
高马赫数  超燃冲压发动机  热化学非平衡  超声速燃烧  低雷诺数流动  激波风洞  飞行试验