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| Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors: Chen Q(陈强); Chen LH(陈立红) ; Gu HB(顾洪斌); Zhang XY(张新宇); Wang P
 View |  Adobe PDF(759Kb) |  Favorite | View/Download：580/189 | Submit date：2014/03/11
Combustion Mode Scramjet Artificial Neural Network |
| A coupled heat transfer analysis with effects of thermal/catalytic cracking of kerosene for regenerative cooled supersonic combustor 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors: Wang X(王曦); Zhong FQ(仲峰泉); Chen LH(陈立红); Zhang XY(张新宇)
View | Adobe PDF(113Kb) | Favorite | View/Download：422/110 | Submit date：2014/04/02
Kerosene Combustor Thermal Regenerative Coupled Catalytic Cracking Analysis Supersonic Transfer Cooled Effects Board Solving Extra Through Differ Energy Cooling Model |
| 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
Authors: 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)
View | Adobe PDF(677Kb) | Favorite | View/Download：630/201 | Submit date：2014/02/24 |
| 自由射流台喷管出口参数的吸收光谱诊断 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors: 李飞; 余西龙; 李东霞; 陈立红; 张新宇
Adobe PDF(1474Kb) | Favorite | View/Download：537/153 | Submit date：2014/01/23
自由射流台 可调谐二极管吸收光谱技术(Tdlas) 温度测量 |
| 超声速气流中横向射流穿透深度半经验公式的推导与修正 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors: 田璐; 李长亮; 陈立红
Adobe PDF(604Kb) | Favorite | View/Download：723/244 | Submit date：2014/01/23
超声速混合 动量交换 半经验公式 穿透深度 |
| Analyses of supersonic combustion by gas sampling 会议论文
13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy, May 16, 2005 - May 20, 2005
Authors: Chen LH(陈立红); Lin R; Gu HB(顾洪斌); Chang XY(张新宇)
View | Adobe PDF(93Kb) | Favorite | View/Download：216/87 | Submit date：2017/06/01
Combustion Efficiency Gas Sampling Probe Sampling Scramjet |
| Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors: Chang XY(张新宇); Chen LH(陈立红); Yu G(俞刚); Qian DX(钱大兴)
View | Adobe PDF(872Kb) | Favorite | View/Download：226/83 | Submit date：2017/06/01
Chinese Academy Of Sciences Enthalpy Flow Hypersonic Propulsion Test Facility Performance Tests Scramjet Testing Supersonic Combustion Total Pressure Total Temperatures |
