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Technologies and Applications of Pipeline-type Oil-gas-water Separation 会议论文
International Conference on Acoustics, Fluid Mechanics and Engineering and the 12th Green's Function Seminar (AFME&GFS 2022), Nanjing, China, 25/11/2022 - 27/11/2022
作者:  Zhang J(张军);  Su,Lide;  Han,Jipu;  Sa,Qier;  Wang,Juntao;  Chai,Weichen;  Li,Bingyu;  Zhong XF(钟兴福)
Adobe PDF(795Kb)  |  收藏  |  浏览/下载：96/24  |  提交时间：2023/05/22
De-oiling Test of New Type Cyclone for Treatment of Wastewater Containing Polymer 会议论文
2020 International Symposium on Geographic Information, Energy and Environmental Sustainable Development, GIEES 2020, Xiamen, China, 26 December 2020 - 27 December 2020
作者:  Wang,Qiang;  Li,Guisheng;  Li,Deqiang;  Li,Gang;  Zhang J(张军);  Zhong XF(钟兴福)
收藏  |  浏览/下载：193/0  |  提交时间：2021/06/21
Parametric Vibration of Top-tensioned Risers with Internal Flow 会议论文
Twenty-ninth (2019) International Ocean and Polar Engineering Conference, Honolulu, Hawaii, USA, June 16-21, 2019
作者:  Yu FJ(于法军);  Xie BQ(谢瑸埼);  Wu H(吴晗);  Wang Q(王琪);  Shi HM(史禾慕);  Zeng XH(曾晓辉)
浏览  |  Adobe PDF(930Kb)  |  收藏  |  浏览/下载：198/42  |  提交时间：2019/10/21
Top-tensioned Riser  Ttr  Parametric Vibration  Internal Flow  Instability Analysis  Hill Equation  
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1120Kb)  |  收藏  |  浏览/下载：486/103  |  提交时间：2018/12/26
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载：391/146  |  提交时间：2018/06/06
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：439/216  |  提交时间：2018/01/16
Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载：308/101  |  提交时间：2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:  Cheng D(程迪);  Wang J(王晶);  Gong J;  Lu Y(陆阳);  Yao W(姚卫);  Li L(李龙);  Fan XJ(范学军);  Fan, Xuejun (xfan@imech.ac.cn)
Adobe PDF(2131Kb)  |  收藏  |  浏览/下载：321/122  |  提交时间：2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures  
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
作者:  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)  |  收藏  |  浏览/下载：425/90  |  提交时间：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
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：472/172  |  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