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| 多股射流撞击雾化机理的实验研究 学位论文 博士论文,北京: 中国科学院大学, 2024 Authors: 侯林![](/image/person.jpg)
Adobe PDF(9995Kb)  |   Favorite  |  View/Download:21/3  |  Submit date:2024/06/11 多股射流 雾化机理 偏心撞击 SMD 液滴分布均匀性 |
| RelaxNet: A structure-preserving neural network to approximate the Boltzmann collision operator 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2023, 卷号: 490, 页码: 112317 Authors: Xiao TB(肖天白); Frank, Martin
Adobe PDF(5203Kb)  |   Favorite  |  View/Download:47/2  |  Submit date:2023/09/05 Kinetic theory Computational fluid dynamics Scientific machine learning Artificial neural network |
| 微波辅助燃烧的数值模型构建和超声速实验研究 学位论文 硕士论文,北京: 中国科学院大学, 2023 Authors: 任耀辉![](/image/person.jpg)
Adobe PDF(74439Kb)  |   Favorite  |  View/Download:142/7  |  Submit date:2023/06/29 微波辅助燃烧 火焰速度增加 动力学效应 超声速燃烧 微波频率 |
| Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文 Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229 Authors: Wang Y(王粤) ; Wang YP(汪运鹏) ; Wang C(王春) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(5479Kb)  |   Favorite  |  View/Download:462/87  |  Submit date:2022/08/24 Multistage Launch Vehicle Aerodynamic Characteristics Shock Wave Interaction Angle of Attack Waverider Boundary Layer Flow Total Variation Diminishing Adverse Pressure Gradient Hypersonic Flows Hypersonic Wind Tunnels |
| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文 Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995 Authors: Wang Y(王粤) ; Wang YP(汪运鹏) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(9707Kb)  |   Favorite  |  View/Download:355/102  |  Submit date:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文 AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946 Authors: Wang Y(王粤) ; Wang YP(汪运鹏) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(2434Kb)  |   Favorite  |  View/Download:348/100  |  Submit date:2022/08/23 Aerodynamic Coefficients Two Stage to Orbit Aerodynamic Performance Hypersonic Flight Hypersonic Wind Tunnels Solenoid Valves Oblique Shock Pneumatic Actuator Hypersonic Flows Computer Aided Engineering |
| GPU 加速的超大规模可压缩湍流直接数值模拟研究 学位论文 博士论文,北京: 中国科学院大学, 2022 Authors: 党冠麟![](/image/person.jpg)
Adobe PDF(39646Kb)  |   Favorite  |  View/Download:517/17  |  Submit date:2023/02/06 软件,湍流,高超声速,直接数值模拟,图形处理器 |
| 非平衡等离子体辅助ADN基推进剂分解及燃烧的光学诊断研究 学位论文 博士论文,北京: 中国科学院大学, 2022 Authors: 王方仪![](/image/person.jpg)
Adobe PDF(7209Kb)  |   Favorite  |  View/Download:241/11  |  Submit date:2023/01/15 ADN基液体推进剂,等离子体助燃,电子温度,电子密度,光学诊断 |
| Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文 International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410 Authors: Meng Y(孟宇) ; Gu HB(顾洪斌) ; Zhang XY(张新宇)![](/image/person.jpg)
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| Advances in Plasma Diagnostics and Applications 专著 Beijing:MDPI, 2022 Authors: Editors:Chen ZT; Attri P; Wang Q(汪球)
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