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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
作者:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
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Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
A high performance fifth-order multistep WENO scheme 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2019, 卷号: 91, 期号: 4, 页码: 159-182
作者:  Ceng FJ(曾方军);  Shen YQ(申义庆);  Liu SP(刘升平);  Liu, L
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critical point  high performance  low-dissipation  multistep WENO scheme  transition point  
Numerical study of the pressure wave-induced shedding mechanism in the cavitating flow around an axisymmetric projectile via a compressible multiphase solver 期刊论文
OCEAN ENGINEERING, 2019, 卷号: 187, 页码: 9
作者:  Ye BS(叶秉晟);  Wang YW(王一伟);  Huang CG(黄晨光);  Huang J(黄荐)
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Cavitation  Compressibility  Shedding mechanism  OpenFOAM (R)  
External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
作者:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
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A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
作者:  Peng J(彭俊);  Zhang ZJ(张子健);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
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Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow  
Analysis of Aerodynamic Noise Characteristics of High-Speed Train Pantograph with Different Installation Bases 期刊论文
APPLIED SCIENCES-BASEL, 2019, 卷号: 9, 期号: 11, 页码: 21
作者:  Yao YF(姚永芳);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P
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high-speed train  pantograph  aerodynamic noise  large eddy simulation  acoustic finite element method  
Numerical simulation of the interaction of two shear layers in double backward-facing steps 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15
作者:  Deng F(邓放);  Han GL(韩桂来);  Liu MK(刘美宽);  Ding, J;  Weng, PF;  Jiang ZL(姜宗林)
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Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme 期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118
作者:  Chen S;  Sun QH(孙泉华);  Klioutchnikov I;  Olivier H
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Shock wave/boundary-layer interactions  Real gas effects  Chemical nonequilibrium  High-order scheme  
Hypervelocity Test with a Detonation-Driven Expansion Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭峻);  Jiang ZL(姜宗林)
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The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Li XD(李旭东);  Shi CM(师曾敏)
浏览  |  Adobe PDF(376Kb)  |  收藏  |  浏览/下载:339/63  |  提交时间:2020/01/06