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基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
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高超声速进气道  不起动  再起动  主动射流  流动控制  
煤粉气流着火机理及最佳煤粉浓度的分析 期刊论文
燃烧科学与技术, 2022, 卷号: 28, 期号: 06, 页码: 639-651
Authors:  魏小林
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煤粉气流  着火机理  最佳煤粉浓度  理论分析  
Density Functional Theory Calculations of Equilibrium Mo Isotope Fractionation Factors among MoOxS4-x2- Species in the Aqueous Phase by the ONIOM Method 期刊论文
ACS EARTH AND SPACE CHEMISTRY, 2022, 页码: 14
Authors:  He YY(何雨旸);  Gao,Caihong;  Wei,Wei;  Liu,Yun
Adobe PDF(3228Kb)  |  Favorite  |  View/Download：450/285  |  Submit date：2023/02/03
paleoredox proxy  ab initio molecular dynamics  implicit solvent model  dispersion correction  water-droplet  periodical boundary condition  
Experimental study of the spray characteristics of twin-fluid atomization: Focusing on the annular flow regime 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 21
Authors:  Liu C(刘畅);  Wu K(吴坤);  Zhang, Zhenyu;  Yuan YM(袁越明);  Fan XJ(范学军)
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Effect of interaction strength on recovery downstream of incident shock interactions 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 27
Authors:  Tong FL(童福林);  Lai, Jiang;  Duan JY(段俊亦);  Dong, Siwei;  Yuan, Xianxu;  Li XL(李新亮)
Adobe PDF(9700Kb)  |  Favorite  |  View/Download：162/31  |  Submit date：2023/02/07
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：329/88  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Effects of injection parameters on propagation patterns of hydrogen-fueled rotating detonation waves 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2022, 卷号: 47, 期号: 91, 页码: 38811-38822
Authors:  Yao KP(姚克鹏);  Yang PF(杨鹏飞);  Teng, Honghui;  Chen, Zheng;  Wang C(王春)
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Rotating detonation wave  Incomplete mixing  Injection parameters  
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
Authors:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
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Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Effects of swirl injection on the combustion of a 11el composite hybrid rocket fuel grain 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182
Authors:  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Luo JX(罗家枭);  Fang SH(方思晗);  Zhang CY;  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(9227Kb)  |  Favorite  |  View/Download：130/33  |  Submit date：2022/10/23
Hybrid rocket engine  Swirl injection  11el composite fuel grain  Regression rate  Oxidizer-to-fuel ratio