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Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
作者:  Yao W(姚卫)
浏览  |  Adobe PDF(9586Kb)  |  收藏  |  浏览/下载:645/293  |  提交时间:2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Subgrid-scale model for large-eddy simulation of transition and turbulence in compressible flows 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 12, 页码: 14
作者:  Zhou H(周浩);  Li XL(李新亮);  Qi H(齐涵);  Yu ZP(于长平)
Adobe PDF(2907Kb)  |  收藏  |  浏览/下载:382/89  |  提交时间:2020/06/15
Discontinuity-Detecting Method for a Four-Point Stencil and Its Application to Develop a Third-Order Hybrid-WENO Scheme 期刊论文
JOURNAL OF SCIENTIFIC COMPUTING, 2019, 卷号: 81, 期号: 3, 页码: 1732-1766
作者:  Liu SP(刘升平);  Shen YQ(申义庆)
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Third-order WENO scheme  Discontinuity-detecting method  Non-nodal critical point  Hybrid-WENO scheme  
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  
超声速膨胀角入射激波/湍流边界层干扰直接数值模拟研究 期刊论文
航空学报, 2019, 页码: 21
作者:  童福林;  孙东;  袁先旭;  李新亮
Adobe PDF(1603Kb)  |  收藏  |  浏览/下载:192/66  |  提交时间:2019/12/16
激波/湍流边界层干扰  膨胀角  本征正交分解  直接数值模拟  
Numerical study of wedge-induced oblique detonations in unsteady flow 期刊论文
JOURNAL OF FLUID MECHANICS, 2019, 卷号: 876, 页码: 264-287
作者:  Yang PF(杨鹏飞);  Ng HD;  Teng HH(滕宏辉)
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detonations  
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 convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
Adobe PDF(4075Kb)  |  收藏  |  浏览/下载:295/86  |  提交时间:2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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
作者:  Zhang ZJ(张子健);  Wen CY;  Liu YF(刘云峰);  Zhang DL(张德良);  Jiang ZL(姜宗林)
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Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation  
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
作者:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
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Scramjet Combustor Mode Transition Liquid Kerosene Acceleration