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A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
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Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
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  
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:  Tong FL(童福林);  Li XL(李新亮);  Duan, Yanhui;  Yu ZP(于长平);  Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li GL(李广利);  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ(徐应洲)
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Aerodynamics  Angle Of Attack  Angle Of Attack Indicators  Boundary Layers  Drag  Drag Coefficient  High Pressure Effects  Hypersonic Aerodynamics  Hypersonic Flow  Spacecraft  
Study on Compression Surface Deformation of Waveriders 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Xu YZ(徐应洲);  Cui K(崔凯);  Li GL(李广利);  Xiao Y(肖尧)
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Aerodynamic Configurations  Aerodynamics  Computational Fluid Dynamics  Deformation  Evolutionary Algorithms  Fluid Dynamics  Hypersonic Aerodynamics  Optimization  Spacecraft  
Elite bases regression: A real-time algorithm for symbolic regression 会议论文
13th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery, ICNC-FSKD 2017, Guilin, Guangxi, China, July 29, 2017 - July 31, 2017
Authors:  Chen C(陈辰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Data mining  Fuzzy systems  Genetic algorithms  Genetic programming  Iterative methods  Learning systems  Comparative studies  Correlation coefficient  Function extraction  Large  scale problem  Machine learning methods  Real time algorithms  Symbolic regression  Symbolic regression problems  
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
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Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
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Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
THE AERODYNAMIC CHARACTERISTICS OF THE PANTOGRAPH WHEN THE TRAIN PASSES THROUGH THE TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:  Guo DL(郭迪龙);  Liu W;  Song JH(宋军浩);  Zhang Y;  Yang GW(杨国伟);  Guo, DL (reprint author), Chinese Acad Sci, Inst Mech, Beijing, Peoples R China.
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