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受限空间斜爆轰宏观结构及其稳定性研究 学位论文
硕士论文,北京: 中国科学院大学, 2020
Authors:  马嘉文
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斜爆轰,受限空间,稳定性,马赫反射,数值模拟  
微波对超声速燃烧火焰结构的影响 期刊论文
航空学报, 2019, 卷号: 40, 期号: 12, 页码: 88-96
Authors:  孟宇;  顾洪斌;  张新宇
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超燃冲压发动机  超声速燃烧  火焰结构  微波  火焰边界  分形几何  
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
Authors:  Yao W(姚卫)
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Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
单空泡与自由液面相互作用规律研究进展 期刊论文
力学学报, 2019, 卷号: 51, 期号: 06, 页码: 1682-1698
Authors:  郭文璐;  李泓辰;  王静竹;  王一伟;  黄晨光
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非球形演化  自由面变形  细射流  粗射流  冠状水裙  
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:26/3  |  Submit date:2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  孟宇
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超燃冲压发动机,燃烧模态,火焰结构,加速过程,微波,滑移电弧,等离子体  
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
Authors:  Yang PF(杨鹏飞);  Ng HD;  Teng HH(滕宏辉)
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detonations  
DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9
Authors:  Fu YW(符耀威);  Yu ZP(于长平);  Yan Z(闫正);  Li XL(李新亮)
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Supersonic combustion  Turbulence jet  Direct numerical simulations  Coherent structures  
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)
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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
Authors:  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