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Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
作者:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
浏览  |  Adobe PDF(824Kb)  |  收藏  |  浏览/下载:226/64  |  提交时间:2017/09/04
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
浏览  |  Adobe PDF(1674Kb)  |  收藏  |  浏览/下载:429/111  |  提交时间:2014/02/24
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
作者:  Zhong FQ(仲峰泉);  Chen TY(陈同银);  Fan XJ(范学军);  Chen LH(陈立红);  Zhang XY(张新宇);  Zhong FQ(仲峰泉)
浏览  |  Adobe PDF(2023Kb)  |  收藏  |  浏览/下载:540/112  |  提交时间:2014/02/24
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
Adobe PDF(6469Kb)  |  收藏  |  浏览/下载:425/98  |  提交时间:2014/02/24
Modeling and measurements of heat release distributions in dual-mode scramjet combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Tian L(田璐);  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian L(田璐)
浏览  |  Adobe PDF(677Kb)  |  收藏  |  浏览/下载:613/195  |  提交时间:2014/02/24
基于释热前推的双模态燃烧室模型研究 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  田璐;  陈立红;  陈强;  张新宇
Adobe PDF(1029Kb)  |  收藏  |  浏览/下载:418/137  |  提交时间:2014/01/23
隔离段模型  释热分布  双模态燃烧室  一维分析  
局部收缩比处处一致的变截面高超声速内转式进气道设计方法 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  肖雅彬;  岳连捷;  高占彪;  陈立红;  张新宇
Adobe PDF(2046Kb)  |  收藏  |  浏览/下载:553/222  |  提交时间:2014/01/23
优化NURBS内转式进气道设计与流场研究 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  肖雅彬;  岳连捷;  陈立红;  张新宇
Adobe PDF(1354Kb)  |  收藏  |  浏览/下载:559/205  |  提交时间:2014/01/23
高超声速  进气道  内转式  边界层抽吸  
高超声速二元进气道循环气流边界层控制方法研究 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  岳连捷;  叶青;  张晓嘉;  陈立红;  张新宇
Adobe PDF(837Kb)  |  收藏  |  浏览/下载:429/206  |  提交时间:2014/01/23
高超声速进气道  边界层分离  流动控制  循环气流控制  
Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
作者:  Li F(李飞);  Yu XL(余西龙);  Gu HB(顾洪斌);  Li Z(李智);  Chen LH(陈立红);  Zhang XY(张新宇);  Li F(李飞)
浏览  |  Adobe PDF(420Kb)  |  收藏  |  浏览/下载:593/197  |  提交时间:2014/02/24