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JF12复现风洞平板边界层转捩研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors:  刘美宽;  韩桂来;  姜宗林
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激波风洞  边界层  转捩  
基于建表技术的化学加速并行算法在气相爆轰数值模拟中的应用 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors:  董刚;  吴锦涛;  刘云峰
View  |  Adobe PDF(1358Kb)  |  Favorite  |  View/Download:183/45  |  Submit date:2019/11/21
建表  化学加速  气相爆轰  计算精度和效率  数值模拟  
Numerical Study of Hydrogen–Air Detonation in Vibrational Non-equilibrium 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Shi, L. S.;  Zhang, P.;  Wen, C. Y.;  Shen, H.;  Parsani, M.;  张德良
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Multiple structure in oxy-hydrogen detonation propagation in rectangular tubes with an improved CE/SE scheme 会议论文
The 2nd International Symposium on Application of Materials Science and Energy Materials, Shanghai, China., December 17-18, 2018
Authors:  ShenY;  Chen P;  Zhang DL(张德良)
View  |  Adobe PDF(1497Kb)  |  Favorite  |  View/Download:196/60  |  Submit date:2019/05/30
Spectral Radiant Intensity Calculation of Air in Shock Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Lyu, Jun Ming;  Cheng, X. L.;  Yu, J. J.;  Li F(李飞);  Yu XL(余西龙)
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On hybrid electroosmotic kinetics for field-effect-reconfigurable nanoparticle trapping in a four-terminal spiral microelectrode array 会议论文
2nd International Conference of Microfluidics, Nanofluidics and Lab-on-a-Chip, Beijing, PEOPLES R CHINA, JUN 08-10, 2018
Authors:  Ren YK;  Song CL;  Liu WY;  Jiang TY;  Song JN;  Wu QS;  Jiang HY
View  |  Adobe PDF(2031Kb)  |  Favorite  |  View/Download:314/130  |  Submit date:2019/04/19
AC field-effect flow control  hybrid electroosmotic kinetics  induced-charge electrokinetic  microfluidics  nanoparticle concentration  
Prediction methods of key development indexes of large gas fields based on big data analysis 会议论文
International Petroleum Technology Conference, Beijing, China, 2019-3.26-28
Authors:  Sun YP;  Guan CX;  Zhang JP;  Li QJ;  Lu JL;  Tang HJ;  Shen WJ(沈伟军);  Li HB;  Zhang HW
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适用于超声速边界层转捩的大涡模拟模型与方法 会议论文
北京力学会第二十五届学术年会, 中国北京, 2019年1月6日
Authors:  于长平;  周浩;  李新亮
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大涡模拟模型  螺旋度  转捩预测  超声速  平板边界层  
Investigation of high-order cell-centered finite difference method for aeroacoustics 会议论文
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, Netherlands, May 20, 2019 - May 23, 2019
Authors:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
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Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Yao W(姚卫);  Li B(李波)
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Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction