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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
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download:347/121  |  Submit date:2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40
Authors:  Zhang ZJ(张子健);  Wen CY;  Liu YF(刘云峰);  Zhang DL(张德良);  Jiang ZL(姜宗林)
View  |  Adobe PDF(4374Kb)  |  Favorite  |  View/Download:412/142  |  Submit date:2019/09/09
Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation  
Construction of bi-layer biluminophore fast-responding pressure sensitive coating for non-contact unsteady aerodynamic testing 期刊论文
POLYMER TESTING, 2019, 卷号: 77, 页码: 8
Authors:  Yang D;  Ren JK;  Li JW(栗继伟);  Wang QL;  Wang Q(汪球);  Xie Z;  Qu XZ
View  |  Adobe PDF(2608Kb)  |  Favorite  |  View/Download:1033/798  |  Submit date:2019/11/25
Pressure sensitive paint (PSP)  Bi-layer structured coating  Fast-response  Self-referenced measurement  
Investigation on the cycle performance and the combustion characteristic of two CO2-based binary mixtures for the transcritical power cycle 期刊论文
ENERGY, 2019, 卷号: 179, 页码: 454-463
Authors:  Pan LS(潘利生);  Ma YJ;  Li T(李腾);  Li HX(李慧鑫);  Li B;  Wei XL(魏小林)
View  |  Adobe PDF(1691Kb)  |  Favorite  |  View/Download:258/78  |  Submit date:2019/09/09
CO2-Based mixtures  Transcritical power cycle  Waste heat recovery  Flammability  
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
Authors:  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  
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
Authors:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
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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
Authors:  Deng F(邓放);  Han GL(韩桂来);  Liu MK(刘美宽);  Ding, J;  Weng, PF;  Jiang ZL(姜宗林)
View  |  Adobe PDF(5760Kb)  |  Favorite  |  View/Download:551/86  |  Submit date:2019/10/21
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
Authors:  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  
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
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Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent  
Experimental investigation of liquid film cooling in hypersonic flow 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
Authors:  Yuan CK(苑朝凯);  Li JP(李进平);  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
Adobe PDF(4383Kb)  |  Favorite  |  View/Download:449/128  |  Submit date:2019/06/10