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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![](/image/person.jpg)
Adobe PDF(65313Kb)  |   Favorite  |  View/Download:531/8  |  Submit date:2023/01/11 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![](/image/person.jpg)
Adobe PDF(7371Kb)  |   Favorite  |  View/Download:586/18  |  Submit date:2022/06/20 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![](/image/person.jpg)
Adobe PDF(1632Kb)  |   Favorite  |  View/Download:204/56  |  Submit date:2022/06/10 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)![](/image/person.jpg)
Adobe PDF(4178Kb)  |   Favorite  |  View/Download:344/84  |  Submit date:2021/11/15 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)![](/image/person.jpg)
Adobe PDF(4108Kb)  |   Favorite  |  View/Download:348/56  |  Submit date:2021/09/07 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
Adobe PDF(5483Kb)  |   Favorite  |  View/Download:179/52  |  Submit date:2022/10/25 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![](/image/person.jpg)
Adobe PDF(11425Kb)  |   Favorite  |  View/Download:431/10  |  Submit date:2021/06/11 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![](/image/person.jpg)
Adobe PDF(6510Kb)  |   Favorite  |  View/Download:261/16  |  Submit date:2021/06/03 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)![](/image/person.jpg)
Adobe PDF(8067Kb)  |   Favorite  |  View/Download:432/84  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |