Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-9 of 9 Help

Filters                            
Selected(0)Clear Items/Page:    Sort:
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：79/13  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
Authors:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
Adobe PDF(2961Kb)  |  Favorite  |  View/Download：248/51  |  Submit date：2022/02/17
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  Favorite  |  View/Download：310/77  |  Submit date：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：372/133  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download：557/183  |  Submit date：2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
View  |  Adobe PDF(2110Kb)  |  Favorite  |  View/Download：401/143  |  Submit date：2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download：408/108  |  Submit date：2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods 期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
View  |  Adobe PDF(1133Kb)  |  Favorite  |  View/Download：1001/267  |  Submit date：2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference  
Theoretical analysis of effects of boundary layer bleed on scramjet thrust 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
Authors:  Yue LJ(岳连捷);  Xu XK(徐显坤);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(788Kb)  |  Favorite  |  View/Download：907/267  |  Submit date：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust