Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 13 Help

Filters        
Selected(0)Clear Items/Page:    Sort:
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)
Adobe PDF(445Kb)  |  Favorite  |  View/Download：465/95  |  Submit date：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
Near-limit instabilities of concurrent flame spread over thin solid fuel 会议论文
10th Asia-Pacific Conference on Combustion, Beijing, China, July 19, 2015 - July 22, 2015
Authors:  Wang SF(王双峰);  Wang SD;  Zhu KC;  Xiao Y;  Lu ZB
Favorite  |  View/Download：145/0  |  Submit date：2016/10/27
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)
View  |  Adobe PDF(824Kb)  |  Favorite  |  View/Download：248/72  |  Submit date：2017/09/04
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)
Adobe PDF(1195Kb)  |  Favorite  |  View/Download：495/179  |  Submit date：2016/07/01
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)
View  |  Adobe PDF(728Kb)  |  Favorite  |  View/Download：292/94  |  Submit date：2017/05/05
Comparative Studies  Flow Charac  Teristics  High Order Harmonics  High Resolution  Instability Modes  Near  Field Structure  Shock Structure  Under  Expanded Jets  
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)
Adobe PDF(590Kb)  |  Favorite  |  View/Download：388/95  |  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  
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism 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:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
Adobe PDF(496Kb)  |  Favorite  |  View/Download：261/76  |  Submit date：2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions  
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)
Adobe PDF(303Kb)  |  Favorite  |  View/Download：213/48  |  Submit date：2017/05/05
Axisymmetric Jet  Flow Parameters  Linear Frequency Response  Mixing Enhancement  Periodic Excitations  Supersonic Circular Jet  Supersonic Combustion  Supersonic Jets  
Numerical simulation of CO reaction with HCl addition based on reduced reaction mechanism 会议论文
10th Asia-Pacific Conference on Combustion, ASPACC 2015, Beijing, China, July 19, 2015 - July 22, 2015
Authors:  Guo XF(郭啸峰);  Wei XL(魏小林);  Li S(李森);  Wei, Xiaolin (xlwei@imech.ac.cn)
Favorite  |  View/Download：194/0  |  Submit date：2017/05/05
Cfd Simulations  Minor Elements  Oh Formation  Oxygen  Rich Conditions  Reaction Mechanism  Reduced Mechanisms  Temperature Increase  Trace Amounts  
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：469/164  |  Submit date：2015/09/29
Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme