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The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
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Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Numerical study of conjugate heat transfer of supercritical kerosene flow in rectangular cooling channel 会议论文
15th International Heat Transfer Conference, IHTC 2014, Kyoto, Japan, August 10, 2014 - August 15, 2014
Authors:  Zhong FQ(仲峰泉);  Dang GX(党国鑫);  Xing YF(邢云绯);  Chen LH(陈立红);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
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Conjugate Heat Transfer  Heat Conduction Equations  Numerical Study  Pseudo-critical Temperature  Rectangular Cooling Channels  Supercritical Kerosenes  Thermodynamic And Transport Properties  Turbulent Transports  
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：421/110  |  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  
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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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：627/199  |  Submit date：2014/02/24
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
Authors:  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)
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Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:  Gu HB(顾洪斌);  Li Z(李智);  Li F(李飞);  Chen LH(陈立红);  Gu SL(顾声龙);  Zhang XY(张新宇);  Gu HB(顾洪斌)
View  |  Adobe PDF(242Kb)  |  Favorite  |  View/Download：562/213  |  Submit date：2014/02/24
溢流槽道位置对二元高超声速进气道性能研究 会议论文
第二届高超声速科技学术会议, 安徽·黄山
Authors:  张晓嘉;  岳连捷;  陈立红;  张新宇
Adobe PDF(5127Kb)  |  Favorite  |  View/Download：497/128  |  Submit date：2010/11/25