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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
作者:  Yang L;  岳连捷;  张启帆;  张新宇
Adobe PDF(1289Kb)  |  收藏  |  浏览/下载：205/50  |  提交时间：2021/01/12
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：249/74  |  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  
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
Adobe PDF(6469Kb)  |  收藏  |  浏览/下载：428/98  |  提交时间：2014/02/24
Design of Base Flow for Streamline-Traced Hypersonic Inlet 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, Bremen, Germany, 19 October 2009 - 22 October 2009
作者:  Yue LJ(岳连捷);  Xiao YB;  Chen LH(陈立红);  Chang XY(张新宇)
浏览  |  Adobe PDF(472Kb)  |  收藏  |  浏览/下载：210/83  |  提交时间：2017/06/01
Investigation on a truncated streamline-traced hypersonic Busemann inlet 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Gong P;  Chang XY(张新宇)
浏览  |  Adobe PDF(3472Kb)  |  收藏  |  浏览/下载：208/84  |  提交时间：2017/06/01
Boundary Layer Corrections  Busemann Inlet  Core Flow  Correction Method  Design Points  Finite Differential Methods  Internal Contraction Ratio  Internal Flows  Mass Flow  
Research on three-dimensional scramjet inlet 会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
作者:  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Chen LH(陈立红);  Xiang AY(向安宇);  Zhang XY(张新宇)
浏览  |  Adobe PDF(1265Kb)  |  收藏  |  浏览/下载：245/73  |  提交时间：2015/09/21
Research on three-dimensional scramiet inlet 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者:  Yue LJ(岳连捷);  Chen LH(陈立红);  Xiao YB;  Gong P;  Chang XY(张新宇)
浏览  |  Adobe PDF(1267Kb)  |  收藏  |  浏览/下载：138/46  |  提交时间：2017/06/01
Capture Ratio  Mass Flow  Surface Oil Dot Visualization  Three-dimensional Scramjet Inlet  
Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison 会议论文
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003
作者:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇)
浏览  |  Adobe PDF(4312Kb)  |  收藏  |  浏览/下载：148/63  |  提交时间：2017/06/01
Compressible Navier-stokes  Computational Studies  Experimental Comparison  Experimental Investigations  Flow Charac-teristics  Hypersonic Propulsion Test Facility  Performance Parameters  Scramjet Inlets