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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  
Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
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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  
A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation 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:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
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Comparative Studies  Flow Charac  Teristics  High Order Harmonics  High Resolution  Instability Modes  Near  Field Structure  Shock Structure  Under  Expanded Jets  
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)
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Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow  
An energy integral method analysis of preferred modes and the spreading rates of supersonic circular jets 会议论文
10th Asia-Pacific Conference on Combustion, ASPACC 2015, Beijing, China, July 19, 2015 - July 22, 2015
Authors:  Yu DH;  Gu HB(顾洪斌);  Zhang P;  Zhang, Peng (pengzhang.zhang@polyu.edu.hk)
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Axisymmetric Jet  Flow Parameters  Linear Frequency Response  Mixing Enhancement  Periodic Excitations  Supersonic Circular Jet  Supersonic Combustion  Supersonic 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)
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Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme  
激波风洞脉冲型应变天平的研制 会议论文
北京力学会第21届学术年会暨北京振动工程学会第22届学术年会, 中国北京, 2015-01-11
Authors:  汪运鹏;  刘云峰;  姜宗林
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高超声速激波风洞  气动力测量  应变天平  固有频率  标准模型  动态校准  
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
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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
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Thermal  Vibration  Acoustic  Multi-physics Environment