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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
Authors:  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.
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Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
超声速模型燃烧室中气化煤油喷注研究 期刊论文
推进技术, 2005, 卷号: 26, 期号: 2, 页码: 97-100
Authors:  俞刚;  李建国;  赵震;  王冬
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航空发动机  煤油  射流  超声速燃烧  
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 期刊论文
Proceedings of the Combustion Institute, 2005
Authors:  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.
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Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor 会议论文
AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Sung CJ
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火焰结构的平面激光诱导荧光技术观测 期刊论文
分析测试学报, 2003, 卷号: 22, 期号: 2, 页码: 16-18
Authors:  赵建荣;  杨仕润;  俞刚;  张新宇
Adobe PDF(98Kb)  |  Favorite  |  View/Download:833/350  |  Submit date:2007/06/15
平面激光诱导荧光  氢氧基  C2  C3  火焰结构  单脉冲  
气泡雾化喷嘴液雾特性 期刊论文
推进技术, 2003, 卷号: 24, 期号: 4, 页码: 348-352
Authors:  岳连捷;  俞刚
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气泡  雾化  液雾特性  超音速燃烧  二相流  
Investigation of Vaporized Kerosene Injection in a Supersonic Model Combustor 会议论文
12th AIAA International Space Planes and Hypersonic Systems and Technologies, Norfolk, Virginia, December 15 – 19, 2003
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhao Z;  Zhang XY(张新宇);  Sun CJ;  Yu G(俞刚)
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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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Planar Laser induced Fluorescence Imaging of OH Radical in Supersonic Combustor 会议论文
Conference on Optical Technology and Image Processing for Fluids and Solids Diagnostics 2002, BEIJING, PEOPLES R CHINA, SEP 03-06, 2002
Authors:  Yang SR(杨仕润);  Zhao JR(赵建荣);  Yu G(俞刚);  Zhang XY(张新宇)
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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