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Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors:  Jiang ZL(姜宗林);  Teng, Honghui
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Instability mechanism and discharge regime diagnosis of microthrusters based on plasma properties 期刊论文
APPLIED OPTICS, 2021, 卷号: 60, 期号: 4, 页码: 1021-1030
Authors:  Wang FY(王方仪);  Zhang SH(张少华);  Liu, Yan;  Yu XL(余西龙)
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Electric-Field-Driven Ion Emission from the Free Surface of Room Temperature Ionic Liquids 期刊论文
JOURNAL OF PHYSICAL CHEMISTRY LETTERS, 2021, 卷号: 12, 期号: 1, 页码: 211-216
Authors:  Zhang, Fei;  Jiang XK(蒋玺恺);  Chen, Gaofeng;  He, Yadong;  Hu, Guoqing;  Qiao, Rui
Adobe PDF(2456Kb)  |  Favorite  |  View/Download：223/80  |  Submit date：2021/03/30
Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
Authors:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
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可压缩转捩及湍流的大涡模拟模型与应用 学位论文
博士论文，北京: 中国科学院大学, 2020
Authors:  周浩
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可压缩流动  转捩及湍流  大涡模拟  建模  
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors:  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)
View  |  Adobe PDF(807Kb)  |  Favorite  |  View/Download：388/129  |  Submit date：2018/07/17
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
Authors:  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)
View  |  Adobe PDF(805Kb)  |  Favorite  |  View/Download：432/166  |  Submit date：2018/06/06
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  Favorite  |  View/Download：522/192  |  Submit date：2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients  
An experimental and numerical study of heat transfer from arrays of impinging jets with surface ribs 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2012, 卷号: 134, 期号: 8, 页码: 082201
Authors:  Spring S;  Xing YF(邢云绯);  Weigand B;  Spring, S;  Univ Stuttgart, Inst Aerosp Thermodynam ITLR, Pfaffenwaldring 31, D-70569 Stuttgart, Germany.
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Jet Impingement  Impingement Cooling  Impingement Array  Surface Ribs  Experimental  Numerical  Cfd  Tlc  Liquid-crystal  Cross-flow  Circular Jets  Staggered Arrays  Spent Air  Impingement  Gas  Systems  Models