Chinese | English

Search in the results

IMECH-IR
(Note: the search results are based on claimed items)

Browse/Search Results:  1-4 of 4 Help

Filters                
Selected(0)Clear Items/Page:    Sort:
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Cheng LW(程柳维);  Zhong FQ(仲峰泉);  Wang ZP(王知溥);  Gu HB(顾洪斌);  Ma SG(马素刚);  Zhang XY(张新宇)
View  |  Adobe PDF(517Kb)  |  Favorite  |  View/Download：335/109  |  Submit date：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
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)
View  |  Adobe PDF(496Kb)  |  Favorite  |  View/Download：265/77  |  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  
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:  Zhong FQ(仲峰泉);  Chen TY(陈同银);  Fan XJ(范学军);  Chen LH(陈立红);  Zhang XY(张新宇);  Zhong FQ(仲峰泉)
View  |  Adobe PDF(2023Kb)  |  Favorite  |  View/Download：560/118  |  Submit date：2014/02/24
无需压力数据及总温假设的超燃冲压发动机一维分析模 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  王曦;  仲峰泉;  邢云绯;  陈立红;  张新宇
Adobe PDF(553Kb)  |  Favorite  |  View/Download：533/228  |  Submit date：2014/01/23
超燃冲压发动机  一维分析模型  燃烧  混合  激波与边界层相互作用