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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)
Favorite  |  View/Download：202/0  |  Submit date：2017/05/27
Conjugate Heat Transfer  Heat Conduction Equations  Numerical Study  Pseudo-critical Temperature  Rectangular Cooling Channels  Supercritical Kerosenes  Thermodynamic And Transport Properties  Turbulent Transports  
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：587/190  |  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：429/113  |  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  
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
View  |  Adobe PDF(1674Kb)  |  Favorite  |  View/Download：471/124  |  Submit date：2014/02/24
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)
View  |  Adobe PDF(2023Kb)  |  Favorite  |  View/Download：563/119  |  Submit date：2014/02/24
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：636/202  |  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)
View  |  Adobe PDF(420Kb)  |  Favorite  |  View/Download：620/209  |  Submit date：2014/02/24
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：575/219  |  Submit date：2014/02/24
CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments 会议论文
Asia-Pacific International Symposium on Aerospace Technology, Xian, PEOPLES R CHINA, SEP 13-15, 2010
Authors:  Wan T(万田);  Chen LH(陈立红);  Wang J(王晶);  Fan XJ(范学军);  Zhang XY(张新宇);  Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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A tunable diode-laser absorption spectroscopy (TDLAS) thermometry for combustion diagnostics 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇)
View  |  Adobe PDF(265Kb)  |  Favorite  |  View/Download：388/111  |  Submit date：2017/06/01
Absorption Lines  Combustion Diagnostics  Direct Absorption  Fiber-coupled  Flat Flame Burner  High Sensitivity  Near Infrared  Non-intrusive  Premixed  Scan Rates  Thermocouple Measurements  Tunable Diode Laser Absorption Spectroscopy  Tunable Diode Lasers  Water Vapor Concentration  Water-vapor Absorption