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Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
作者:  Gan JY;  Shen YQ(申义庆);  Zha GC
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Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
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)
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Aerodynamic Forces  Chinese Academy Of Sciences  Different Structure  Digital Filtering  Large  Scale Modeling  Low  Frequency Vibration  Strain Gauge Balances  Strain Gauge Sensors  
Plasma Assisted Low Temperature Combustion 会议论文
22nd International Symposium on Plasma Chemistry (ISPC 22), Antwerp, BELGIUM, JUL 05-10, 2015
作者:  Ju YG;  Lefkowitz JK;  Reuter CB;  Won SH;  Yang XL;  Yang S;  Sun WT;  Jiang ZL(姜宗林);  Chen Q;  Ju, YG (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
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Plasma Assisted Combustion  Low Temperature Chemistry  Kinetics  Cool Flames  S-curve Transition  Nonequilibrium Plasma  Saturated-hydrocarbons  Diffusion Flames  Pulsed Discharge  Ignition  Mixtures  Oxidation  Kinetics  Enhancement  
A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 6, 页码: 1517-1526
作者:  Chen S;  Sun QH(孙泉华)
浏览  |  Adobe PDF(1688Kb)  |  收藏  |  浏览/下载：242/71  |  提交时间：2017/04/26