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携带颗粒各向同性湍流的大涡模拟与亚格子模型 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  周志登
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颗粒拉格朗日弥散  大涡模拟  湍流亚格子模型  颗粒亚格子模型  人工神经网络  有限颗粒雷诺数  
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  
Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors:  Cheng D(程迪);  Wang J(王晶);  Lu Y(陆阳);  Li L(李龙);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(2651Kb)  |  Favorite  |  View/Download:201/42  |  Submit date:2019/09/09
Heat flux measurement  Kerosene  Supersonic combustion  Scramjet  Heat flux sensor  
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
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
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Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
Microgravity diffusion flame spread over a thick solid in step-changed low-velocity opposed flows 期刊论文
COMBUSTION AND FLAME, 2019, 卷号: 205, 页码: 55-67
Authors:  Zhu F(朱凤);  Lu ZB;  Wang SF(王双峰);  Yin YL
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Opposed-flow flame spread  Thick solid  Microgravity  Radiation-controlled regime  Diffusive-thermal instability  
Numerical investigation on bubble dynamics during pool nucleate boiling in presence of a non-uniform electric field by LBM 期刊论文
APPLIED THERMAL ENGINEERING, 2019, 卷号: 155, 页码: 637-649
Authors:  Feng Y;  Li HX;  Guo KK;  Lei XL;  Zhao JF(赵建福)
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Lattice Boltzmann method  Electrohydrodynamics  Bubble departure diameter  Bubble release frequency  
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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Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
Authors:  Wang Q(汪球);  Olivier H;  Einhoff J;  Li JP(李进平);  Zhao W(赵伟)
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Heat transfer measurement  Lateral heat conduction  Shock tunnel  Thermocouple  Hypersonic  
高速飞行器发动机尾焰红外辐射目标特性计算方法 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  丛彬彬
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高速飞行器  高温尾焰  超声速射流  红外辐射  光线追踪  谱线筛选  
不同喷压比下欠膨胀射流对特征频率激励的响应 期刊论文
推进技术, 2019, 卷号: 40, 期号: 06, 页码: 1239-1246
Authors:  李晓鹏;  周蕊;  庄法坤;  曹逻炜;  谢国山;  范学军
View  |  Adobe PDF(6645Kb)  |  Favorite  |  View/Download:147/12  |  Submit date:2019/09/12
欠膨胀射流  喷压比  特征频率激励  大涡模拟  流动响应