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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  
Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
浏览  |  Adobe PDF(3918Kb)  |  收藏  |  浏览/下载:521/165  |  提交时间:2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
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  
Optimization Study on Fluids for the Gravity-Driven Organic Power Cycle 期刊论文
ENERGIES, 2019, 卷号: 12, 期号: 4, 页码: 19
作者:  Shi WX;  Pan LS(潘利生)
浏览  |  Adobe PDF(4283Kb)  |  收藏  |  浏览/下载:586/412  |  提交时间:2019/05/30
gravity driven organic power cycle (GDOPC)  organic Rankine cycle (ORC)  theoretical study  fluid optimization  
Finite-thickness effect of the fluids on bubbles and spikes in Richtmyer-Meshkov instability for arbitrary Atwood numbers 期刊论文
PLASMA SCIENCE & TECHNOLOGY, 2019, 卷号: 21, 期号: 2, 页码: ARUNSP 025001
作者:  Liu WH;  Yu ZP(于长平);  Wang P;  Fu Z;  Wang LL;  Chen YL
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Richtmyer-Meshkov instability  bubbles and spikes  finite-thickness  
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1820Kb)  |  收藏  |  浏览/下载:454/154  |  提交时间:2018/12/27
Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio