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Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles 期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
Authors:  Luo CT(罗长童);  Hu ZM(胡宗民);  Zhang SL;  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Aerodynamic Coefficient  Data Correlation  Scaling Parameter  Genetic Programming  Invariant  
高超声速风洞实验数据的多维空间相关理论与关联方法 期刊论文
中国科学: 物理学 力学 天文学, 2015, 卷号: 45, 期号: 12, 页码: 124705
Authors:  姜宗林;  罗长童;  胡宗民;  刘云峰
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Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Wave system fitting: A new method for force measurements in shock tunnels with long test duration 期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
Authors:  Luo CT(罗长童);  Wang YP(汪云鹏);  Wang C(王春);  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Aerodynamic Force Measurements  Strain Gauge Balance  Inertia Compensation  Signal Decomposition  Accelerometer-free  Shock Tunnels  
Experimental study on convection heat transfer and air drag in sinter layer 期刊论文
JOURNAL OF CENTRAL SOUTH UNIVERSITY, 2015, 卷号: 22, 期号: 7, 页码: 2841-2848
Authors:  Pan LS(潘利生);  Wei XL(魏小林);  Peng Y;  Shi XB;  Liu HL;  Pan, LS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1145Kb)  |  Favorite  |  View/Download：426/79  |  Submit date：2015/10/21
Sinter Layer  Convection Heat Transfer  Pressure Drop  
Relative contribution ratio: A quantitative metrics for multi-parameter analysis 期刊论文
Cogent Mathematics, 2015, 卷号: 2, 期号: 1, 页码: 1068979
Authors:  Luo CT(罗长童);  Jiang ZL(姜宗林);  Wang C(王春);  Hu ZM(胡宗民)
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Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
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Hydrocarbons  Combustors  Cooling  Heat Transfer  
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
Authors:  Dang GX;  Zhong FQ(仲峰泉);  Zhang YJ;  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
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Supercritical Kerosene  Convective Heat Transfer  Turbulent Flow  Numerical Study  
船舶厨余垃圾的热等离子体气化研究 学位论文
硕士论文，北京: 中国科学院大学, 2015
Authors:  李慧鑫
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热等离子体  厨余垃圾  气化  化学平衡  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1112Kb)  |  Favorite  |  View/Download：554/229  |  Submit date：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas