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Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
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Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients  
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
View  |  Adobe PDF(5104Kb)  |  Favorite  |  View/Download：252/48  |  Submit date：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow  
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(590Kb)  |  Favorite  |  View/Download：386/95  |  Submit date：2017/05/05
Frequency Spectrum Analysis  High Temporal Resolution  Instantaneous Flow  Noise Generation Mechanisms  Theoretical Modeling  Three  Dimensional Numerical Studies  Transport Mechanism  Under  Expanded Jets  
A New Flux Splitting Scheme for Euler Equations of Gas Dynamics 会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
Authors:  Li XD(李馨东);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1140Kb)  |  Favorite  |  View/Download：468/163  |  Submit date：2015/09/29
Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme  
Measurements of CO concentration distribution for Mars atmospheric entry by combining OES and TDLAS 会议论文
3rd International Symposium on Laser Interaction with Matter, Nanjing PEOPLES R CHINA, NOV 02-05 2014
Authors:  Lin X(林鑫);  Chen LZ;  Ou DB;  Li F(李飞);  Yu XL(余西龙);  oudongbin@sina.com
View  |  Adobe PDF(1140Kb)  |  Favorite  |  View/Download：448/140  |  Submit date：2015/09/29
Optical Emission Spectroscopy Tunable Diode Laser Absorption Spectroscopy Shock Wave  Temperature  Concentration  
Coupling Analysis for the Thermo-Acoustic-Vibration Response of a Thin-Walled Box 会议论文
10th International Conference on Vibration Engineering and Technology of Machinery, Manchester ENGLAND, SEP 09-11 2014
Authors:  Yang Y(杨焱);  Wu CW(吴臣武);  yangyan@imech.ac.cn
View  |  Adobe PDF(1212Kb)  |  Favorite  |  View/Download：452/132  |  Submit date：2015/09/29
Thermal  Vibration  Acoustic  Multi-physics Environment  
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL;  Xiao Y(肖尧);  Situ M
View  |  Adobe PDF(872Kb)  |  Favorite  |  View/Download：369/158  |  Submit date：2017/05/05
Aero  Dynamic Performance  Aerodynamic Performance Predictions  Design Methodology  Flight Altitudes  Numerical Results  Propulsion System  Turbulent Models  Wing Body Aircraft