IMECH-IR

Browse/Search Results:  1-10 of 71 Help

Filters        
Selected(0)Clear Items/Page:    Sort:
Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Wu WN(邬婉楠);  Zhang QF(张启帆);  Chen H(陈昊)
Favorite  |  View/Download:39/0  |  Submit date:2024/03/11
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download:44/6  |  Submit date:2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Chen H(陈昊);  Zhang QF(张启帆);  He CM(何成明)
Adobe PDF(6058Kb)  |  Favorite  |  View/Download:157/39  |  Submit date:2022/11/28
Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 10, 页码: 15
Authors:  Li YL(李育凌);  Yue LJ(岳连捷);  He CM(何成明);  Wu WN(邬婉楠);  Chen H(陈昊)
Adobe PDF(3520Kb)  |  Favorite  |  View/Download:239/76  |  Submit date:2022/11/14
scramjet inlet  Lagrange optimization method  shock configuration  
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:157/48  |  Submit date:2022/10/23
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:249/45  |  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:290/68  |  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  
Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection 期刊论文
AIAA JOURNAL, 2022, 页码: 5
Authors:  Li JJ(李江江);  Chen H(陈昊);  Tong XT(仝晓通);  Gao X;  Zhang QF(张启帆);  Yue LJ(岳连捷)
Adobe PDF(1812Kb)  |  Favorite  |  View/Download:217/46  |  Submit date:2022/05/17
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:555/103  |  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  
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7
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(1382Kb)  |  Favorite  |  View/Download:155/27  |  Submit date:2022/03/22