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Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:  Li F(李飞);  Yu XL(余西龙);  Tong YG(仝颖刚);  Shen Y(沈岩);  Chen J(陈健);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Scramjet  Kerosene Fuel  Plasma Torch  Ignition  
Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 2, 页码: 416-422
Authors:  Dang GX(党国鑫);  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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考虑煤油裂解效应的超声速燃烧室再生冷却过程分析 期刊论文
推进技术, 2013, 卷号: 34, 期号: 1, 页码: 47-53
Authors:  王曦;  仲峰泉;  陈立红;  张新宇
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超声速燃烧室  耦合传热  再生冷却  超临界态  催化裂解  
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
Authors:  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)
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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
Authors:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
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Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor 期刊论文
Journal of Propulsion and Power, 2003, 卷号: 19, 期号: 5, 页码: 885-893
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Chen LH(陈立红);  Sung CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd, Beijing 100080, Peoples R China.
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Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors 期刊论文
Journal of Propulsion and Power, 2001, 卷号: 17, 期号: 6, 页码: 1263-1272
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Chen LH(陈立红);  Song CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd,Haidian Dist, Beijing 100080, Peoples R China.
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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)
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Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures