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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
作者:  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.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：537/225  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Self-sustained combustion of carbon monoxide promoted by the Cu-Ce/ZSM-5 catalyst in CO/O-2/N-2 atmosphere 期刊论文
Applied Catalysis B-Environmental, 2015, 卷号: 162, 页码: 282-288
作者:  Bin F(宾峰);  Wei XL(魏小林);  Li B(李博);  Hui KS;  Bin, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
浏览  |  Adobe PDF(1904Kb)  |  收藏  |  浏览/下载：850/253  |  提交时间：2014/12/18
Carbon Monoxide  Self-sustained Combustion  Cu-ce/zsm-5  Catalytic Activity  
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
作者:  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)  |  收藏  |  浏览/下载：473/173  |  提交时间：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  
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
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
浏览  |  Adobe PDF(496Kb)  |  收藏  |  浏览/下载：247/74  |  提交时间：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
作者:  Yu DH;  Gu HB(顾洪斌);  Zhang P;  Zhang, Peng (pengzhang.zhang@polyu.edu.hk)
浏览  |  Adobe PDF(303Kb)  |  收藏  |  浏览/下载：200/48  |  提交时间：2017/05/05
Axisymmetric Jet  Flow Parameters  Linear Frequency Response  Mixing Enhancement  Periodic Excitations  Supersonic Circular Jet  Supersonic Combustion  Supersonic Jets  
Characterization of the NO-soot combustion process over La0.8Ce0.2Mn0.7Bi0.3O3 catalyst 期刊论文
Proceedings of The Combustion Institute, 2015, 卷号: 35, 期号: 2, 页码: 2241-2248
作者:  Bin F(宾峰);  Song CL;  Lv G;  Li XD;  Cao XF;  Song JO;  Wu SH;  Song, CL (reprint author), Tianjin Univ, State Key Lab Engines, Tianjin 300072, Peoples R China.
浏览  |  Adobe PDF(1540Kb)  |  收藏  |  浏览/下载：311/80  |  提交时间：2015/03/17
Soot  Nitrous Oxide  Catalytic Combustion  Perovskite Catalyst