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再生冷却通道微结构强化传热与流动机理研究 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  李冼
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再生冷却  航空煤油  凹陷窝  微肋  强化传热  
面向高超声速飞行的激波诱燃宏观流动及微观机理分析 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  马凯夫
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激波诱导燃烧  氢氧燃烧  热化学非平衡  微观机理  激波诱燃发动机  
斜激波串非对称特性研究 期刊论文
推进技术, 2022, 卷号: 43, 期号: 04, 页码: 101-108
Authors:  黄庭隆;  贺理浩;  岳连捷
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隔离段  斜激波串  非对称性  建模分析  数值仿真  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors:  Jiang ZL(姜宗林);  Teng, Honghui
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Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:  Wu CW(吴臣武);  Liu C(刘聪);  Hu DL(胡灯亮);  Liu HL(刘宏立);  Huang HJ(黄河激)
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Strain  Balance  Milli-newton  Design  Calibration  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
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High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
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Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
稀薄来流与连续喷流相互作用的连续性假设失效研究 学位论文
硕士论文,北京: 中国科学院大学, 2021
Authors:  宋杭
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连续性假设失效  非平衡度  喷流与来流相互作用  直接模拟蒙特卡罗方法  
超声速燃烧中射流的尺度效应与燃烧稳定性研究 学位论文
硕士论文,北京: 中国科学院大学, 2021
Authors:  李桢
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超声速燃烧  燃烧室尺度  射流尺度  火焰模式  火焰稳定性  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow