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An Analytical Calculation Method and Mechanical Response Laws of Buried Pipelines Subjected to the Impact of Transverse Landslides 会议论文
International Conference on Applied Mechanics, Materials Physics, and Engineering Structures (MMPES 2023), Wuhan, China, 05/01/2023 - 06/01/2023
作者:  Fan ZY(樊志勇);  Wu,Bin;  Liu TP(刘天苹);  Zhao Y(赵颖);  Liu XY(刘晓宇)
Adobe PDF(1745Kb)  |  收藏  |  浏览/下载：103/31  |  提交时间：2023/07/17
Transverse Landslides  Buried Pipeline  Analytical Method  Mechanical Responses  Influence Factors  
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：384/143  |  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：434/214  |  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  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：294/87  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
不同喷压比下欠膨胀射流对特征频率激励的响应 会议论文
第九届全国流体力学学术会议, 中国江苏南京, 2016-10-20
作者:  李晓鹏;  姚卫;  范学军
浏览  |  Adobe PDF(122Kb)  |  收藏  |  浏览/下载：373/71  |  提交时间：2017/09/27
欠膨胀射流  喷压比  特征频率激励  大涡模拟  流动响应  
Visualization of flow separation inside cut kerf during laser cutting of thick sections 会议论文
34th International Congress on Applications of Lasers and Electro-Optics (ICALEO), Atlanta, GA, OCT 18-22, 2015
作者:  Zhang C;  Wen P;  Yao ZH;  Yuan YM(袁越明);  Fan XJ(范学军);  Wen, P (reprint author), Tsinghua Univ, State Key Lab Tribol, Beijing 100084, Peoples R China.
浏览  |  Adobe PDF(1350Kb)  |  收藏  |  浏览/下载：304/107  |  提交时间：2016/06/28
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：464/170  |  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  
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
作者:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(728Kb)  |  收藏  |  浏览/下载：269/87  |  提交时间：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
作者:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(590Kb)  |  收藏  |  浏览/下载：360/91  |  提交时间：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  
JP-10裂解的激波管实验与动力学模拟 会议论文
中国力学大会-2015, 中国上海, 2015-08-16
作者:  王苏;  熊壮;  范秉诚;  崔季平
浏览  |  Adobe PDF(214Kb)  |  收藏  |  浏览/下载：276/115  |  提交时间：2016/08/16
单脉冲激波管  裂解产物  动力学模拟  甲基环戊烯  Jp-10  环戊二烯  气相色谱法分析  边界层  理想性