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Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation 会议论文
AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020
作者:  Jin Y;  廖飞, Cai JS
Adobe PDF(4611Kb)  |  收藏  |  浏览/下载：194/104  |  提交时间：2021/06/11
Viscous Elastoplastic SPH Model for Long-Distance High-Speed Landslide 会议论文
SPHERIC Beijing International Workshop (SPHERIC Beijing), Peking Univ, Beijing, PEOPLES R CHINA, OCT 17-20, 2017
作者:  Zhang WT(张炆涛);  Shi CQ(石传奇);  An Y(安翼);  Yang SH(杨世豪);  Liu QQ(刘青泉)
浏览  |  Adobe PDF(1105Kb)  |  收藏  |  浏览/下载：215/50  |  提交时间：2019/04/19
Granular solid regime  granular liquid regime  viscous elastoplastic model  
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
作者:  Sun YP;  Guan CX;  Zhang JP;  Li QJ;  Lu JL;  Tang HJ;  Shen WJ(沈伟军);  Li HB;  Zhang HW
浏览  |  Adobe PDF(1130Kb)  |  收藏  |  浏览/下载：183/37  |  提交时间：2019/08/19
A novel method of cooling channel optimization for active-cooled structure using the calculus of variations 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Li X(李轩);  Lu Y(陆阳);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(705Kb)  |  收藏  |  浏览/下载：176/60  |  提交时间：2020/11/20
Development of zone flamelet model for scramjet combustor modeling 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);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：258/87  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：271/81  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
PARAMETRIZATION OF HIGH-SPEED TRAIN STREAMLINE SHAPE 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
作者:  Sun ZX(孙振旭);  Zhang Y;  Yang GW(杨国伟);  Sun, ZX (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
浏览  |  Adobe PDF(1180Kb)  |  收藏  |  浏览/下载：216/77  |  提交时间：2018/01/16
Multiobjective Optimization  Head