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Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载：378/62  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
作者:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  收藏  |  浏览/下载：254/103  |  提交时间：2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
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
作者:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载：331/114  |  提交时间：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene 期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
作者:  Liang JH(梁金虎);  Wang S(王苏);  Zhang ST(张胜涛);  Yue LJ(岳连捷);  Fan BC(范秉诚);  Zhang XY(张新宇);  Cui JP(崔季平);  Wang S(王苏)
浏览  |  Adobe PDF(1351Kb)  |  收藏  |  浏览/下载：885/215  |  提交时间：2014/08/14
Ignition Delay  Vitiation Effect  Kerosene  Water  Carbon Dioxide  Shock Tube  
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
作者:  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)  |  收藏  |  浏览/下载：878/258  |  提交时间：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust  
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1524Kb)  |  收藏  |  浏览/下载：846/231  |  提交时间：2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 期刊论文
Proceedings of the Combustion Institute, 2005
作者:  Yu G(俞刚);  Li JG(李建国);  Zhao JR(赵建荣);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1268Kb)  |  收藏  |  浏览/下载：939/287  |  提交时间：2007/06/15
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 会议论文
30th International Symposium on Combustion, JUL 25-30, 2004 Univ Illinois Chicago, Chicago, IL
作者:  Yu G(俞刚);  Li JG(李建国);  Zhao JR(赵建荣);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Song ZR(宋知人)
Adobe PDF(1268Kb)  |  收藏  |  浏览/下载：786/235  |  提交时间：2007/12/18