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高超声速喷管设计理论与方法 期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors:  汪运鹏;  姜宗林
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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)
Adobe PDF(6207Kb)  |  Favorite  |  View/Download:257/101  |  Submit date:2021/02/09
Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 卷号: 192, 期号: 10, 页码: 1931-1945
Authors:  Xiang GX(项高翔);  Yang PF(杨鹏飞);  Teng HH(滕宏辉);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1871Kb)  |  Favorite  |  View/Download:538/155  |  Submit date:2019/09/09
Al particle  cellular detonation  heat capacity  hybrid model  
Energy transport characteristics of converging Richtmyer-Meshkov instability 期刊论文
AIP ADVANCES, 2020, 卷号: 10, 期号: 10, 页码: 12
Authors:  Fu YW(符耀威);  Yu ZP(于长平);  Li XL(李新亮)
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基于第二粘性的Navier-Stokes方程组求解正激波结构 期刊论文
计算物理, 2020, 卷号: 37, 期号: 5, 页码: 505-513
Authors:  李馨东;  赵英奎;  胡宗民;  姜宗林
View  |  Adobe PDF(812Kb)  |  Favorite  |  View/Download:358/80  |  Submit date:2019/12/16
Navier-Stokes方程  Stokes假设  第二粘性  体积粘性,正激波结构  
Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
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Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:  Luo K(罗凯);  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2023Kb)  |  Favorite  |  View/Download:329/105  |  Submit date:2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
Authors:  Zhang SZ(张仕忠);  Wang Q(汪球);  Li JP(李进平);  Zhang XY(张晓源);  Chen H(陈宏)
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calorimeter  shock tunnel  heat transfer measurement  hypersonic  
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
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Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 41, 页码: 21940-21955
Authors:  Yao W(姚卫)
Adobe PDF(3791Kb)  |  Favorite  |  View/Download:276/133  |  Submit date:2020/09/27
Dynamic zone flamelet model  Supersonic hydrogen jet  Large eddy simulation  Supersonic combustion  Turbulent combustion model