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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
作者:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  收藏  |  浏览/下载：147/42  |  提交时间：2022/07/04
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)
Adobe PDF(805Kb)  |  收藏  |  浏览/下载：384/143  |  提交时间：2018/06/06
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
Adobe PDF(4139Kb)  |  收藏  |  浏览/下载：260/55  |  提交时间：2019/04/19
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)
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)
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  
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)
Adobe PDF(6096Kb)  |  收藏  |  浏览/下载：302/86  |  提交时间：2018/01/16
Force measurement in a shock tunnel with 100 milliseconds test duration 会议论文
34th AIAA Applied Aerodynamics Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(6592Kb)  |  收藏  |  浏览/下载：303/78  |  提交时间：2017/05/05
Aerodynamic Forces  Chinese Academy Of Sciences  Different Structure  Digital Filtering  Large  Scale Modeling  Low  Frequency Vibration  Strain Gauge Balances  Strain Gauge Sensors  
Experimental and Modeling Investigation of CO2 Dissociation in Mars Entry Condition 会议论文
18th International Conference on the Methods of Aerophysical Research (ICMAR), Perm Natl Res Polytechn Univ, Perm, RUSSIA, JUN 27-JUL 03, 2016
作者:  Lin X;  Chen LZ;  Peng JL;  Li JP(李进平);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1399Kb)  |  收藏  |  浏览/下载：285/78  |  提交时间：2017/05/12
Nonequilibrium  
A New Flux Splitting Scheme for Euler Equations of Gas Dynamics 会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
作者:  Li XD(李馨东);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
Adobe PDF(1140Kb)  |  收藏  |  浏览/下载：447/153  |  提交时间：2015/09/29
Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme  
Effects of a higher Reynolds number and introduced perforation on flows past the conic cylinder 会议论文
25th International Ocean and Polar Engineering Conference, ISOPE 2015, Kona, Big Island, HI, United states, June 21, 2015 - June 26, 2015
作者:  Lin LM(林黎明);  Zhong XF(钟兴福);  Wu YX(吴应湘)
Adobe PDF(703Kb)  |  收藏  |  浏览/下载：228/87  |  提交时间：2017/05/05
Circular Holes  Conic Disturbance  Disturbance Regime  Drag And Lift Coefficients  Hydrodynamic Parameters  Near Wake  Vortex Induced Vibration  Vortex Pattern