中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共21条，第1-10条 帮助

限定条件    
已选(0)清除 条数/页：   排序方式：
超声速三维进气道内激波干扰的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 6
作者:  项高翔;  王春;  汪运鹏;  姜宗林
浏览  |  Adobe PDF(1393Kb)  |  收藏  |  浏览/下载：467/95  |  提交时间：2017/12/22
高超声速流动  箱式进气道  侧壁压缩进气道  波系结构  流场区域  
分辨率优化的混合WENO格式 期刊论文
计算物理, 2017, 卷号: 35, 期号: 4, 页码: 397-404
作者:  郭元;  田奇;  梁贤;  李新亮
浏览  |  Adobe PDF(614Kb)  |  收藏  |  浏览/下载：230/66  |  提交时间：2018/10/24
混合格式  数值耗散  色散  保单调  优化  
Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
作者:  Li XP(李晓鹏);  Zhou, Rui;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(5723Kb)  |  收藏  |  浏览/下载：416/182  |  提交时间：2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
Initiation structure of oblique detonation waves behind conical shocks 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
作者:  Yang PF(杨鹏飞);  Ng, Hoi Dick;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
浏览  |  Adobe PDF(5788Kb)  |  收藏  |  浏览/下载：449/99  |  提交时间：2017/11/16
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
浏览  |  Adobe PDF(1315Kb)  |  收藏  |  浏览/下载：336/128  |  提交时间：2017/11/29
A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：277/112  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
隔离段抽吸引起的激波迟滞现象研究 期刊论文
推进技术, 2017, 卷号: 38, 期号: 04, 页码: 732-739
作者:  马生虎;  岳连捷;  贾轶楠;  肖雅彬;  张新宇
浏览  |  Adobe PDF(1677Kb)  |  收藏  |  浏览/下载：251/67  |  提交时间：2017/12/22
超燃冲压发动机  隔离段  激波反射迟滞  边界层分离迟滞  
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：440/216  |  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  
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
浏览  |  Adobe PDF(1358Kb)  |  收藏  |  浏览/下载：422/107  |  提交时间：2018/01/16
Computational Fluid Dynamics  Computer Software  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Runge Kutta Methods  Shock Tubes  Shock Waves  Spacecraft  Turbulence  Two Phase Flow  
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