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Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载:65/15  |  提交时间:2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(704Kb)  |  收藏  |  浏览/下载:22/9  |  提交时间:2018/01/16
Spacecraft  
Optimization Design and Performance Analysis of a Miniature Stirling Engine 会议论文
2ND INTERNATIONAL CONFERENCE ON MATERIALS SCIENCE, RESOURCE AND ENVIRONMENTAL ENGINEERING (MSREE 2017), Wuhan, PEOPLES R CHINA, OCT 27-29, 2017
作者:  You ZP;  Yang B;  Pan LS(潘利生);  Hao CS;  You, ZP (reprint author), Shijiazhuang Tiedao Univ, Coll Mech Engn, Shijiazhuang 050043, Hebei, Peoples R China.
浏览  |  Adobe PDF(155Kb)  |  收藏  |  浏览/下载:24/10  |  提交时间:2018/01/16
Miniature Stirling Engine  Isothermal Analysis  Adiabatic Analysis  
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, Hypersonics 2017, 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:54/20  |  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  
Fast Modeling Methods for Complex System with Separable Features 会议论文
2017 10TH INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL INTELLIGENCE AND DESIGN (ISCID), VOL. 1, Hangzhou, PEOPLES R CHINA, DEC 09-10, 2017
作者:  Chen C(陈晨);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(249Kb)  |  收藏  |  浏览/下载:14/3  |  提交时间:2018/06/06
Data-driven Modeling  Genetic Programming  Generalized Separable Model  Multi-level Block Search  
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, Hypersonics 2017, 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)
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Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(6096Kb)  |  收藏  |  浏览/下载:27/0  |  提交时间:2018/01/16
Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文
53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017
作者:  Fan E;  Wu K;  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(2297Kb)  |  收藏  |  浏览/下载:45/13  |  提交时间:2018/01/16
激波-湍流边界层干扰的直接数值模拟研究 会议论文
第七届中国空气动力学学会物理气体动力学专业委员会换届选举大会暨学术交流会论文集, 中国北京, 2016-12-23
作者:  李新亮;  童福林;  朱兴坤
浏览  |  Adobe PDF(654Kb)  |  收藏  |  浏览/下载:55/27  |  提交时间:2017/09/27
湍流边界层  直接数值模拟  流体力学研究  转捩  前沿热点问题  折角  飞行器设计  壁温  湍流模型  气动设计  
声源激励下的声-振耦合响应分析 会议论文
2016年度全国气动声学学术会议论文摘要集, 中国北京, 2016-11-04
作者:  杨焱;  吴臣武
浏览  |  Adobe PDF(287Kb)  |  收藏  |  浏览/下载:67/29  |  提交时间:2017/09/27
振动  声学  热结构  多物理环境