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| 碳氢燃料冲击射流传热特性数值研究 会议论文
中国航天第三专业信息网第三十九届技术交流会暨第三届空天动力联合会, 河南洛阳, 2018年8月22日-25日
Authors: 杜蒙蒙; 仲峰泉 ; 邢云绯; 张新宇
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Impingement Jets cooling Hydrocarbon Fuels Heat Transfer Effectiveness Numerical Study |
| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇)
View | Adobe PDF(517Kb) | Favorite | View/Download：332/108 | Submit date：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| 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 |
| 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 |
