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| 主被动冷却平板结构耦合传热特性研究 学位论文 博士论文,北京: 中国科学院大学, 2023 作者: 胡国豪 Adobe PDF(38874Kb)  |  收藏  |  浏览/下载:118/12  |  提交时间:2023/06/26 主动热防护 主/被动复合热防护 导热热阻 预测模型 热应力 |
| Hybrid PD-DEM approach for modeling surface erosion by particles impact 期刊论文 COMPUTATIONAL PARTICLE MECHANICS, 2023 作者: Walayat, Khuram; Haeri, Sina; Iqbal, Imran; Zhang YH(张勇豪) Adobe PDF(5522Kb)  |  收藏  |  浏览/下载:66/0  |  提交时间:2023/06/15 Peridynamics Discrete element method Multi-particle contact Solid particle erosion Damage Crack |
| 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 作者: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  收藏  |  浏览/下载:363/69  |  提交时间: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 |
| 基于主动射流控制的高超声速进气道再起动性能研究(英文) 期刊论文 Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662 作者: 靳一超; 姚卫 Adobe PDF(1844Kb)  |  收藏  |  浏览/下载:140/36  |  提交时间:2023/02/09 高超声速进气道 不起动 再起动 主动射流 流动控制 |
| 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 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9707Kb)  |  收藏  |  浏览/下载:294/83  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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 作者: 党冠麟 Adobe PDF(39646Kb)  |  收藏  |  浏览/下载:428/15  |  提交时间:2023/02/06 软件,湍流,高超声速,直接数值模拟,图形处理器 |
| Effects of swirl injection on the combustion of a 11el composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 作者: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY; Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  收藏  |  浏览/下载:118/29  |  提交时间:2022/10/23 Hybrid rocket engine Swirl injection 11el composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 作者: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY(张春元); Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  收藏  |  浏览/下载:97/9  |  提交时间:2022/11/08 Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Experimental study of hysteresis and catastrophe in a cavity-based scramjet combustor 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 10, 页码: 118-133 作者: Zhang X(张旭); Zhang QF(张启帆); Wu ZJ(吴振杰); Yue LJ(岳连捷); Gao ZB(高占彪); Luo WH(罗苇航); Chen H(陈昊) Adobe PDF(4834Kb)  |  收藏  |  浏览/下载:28/2  |  提交时间:2023/07/17 Catastrophe Cavity-based scramjet Flame stabilization Flame/shock interaction Hysteresis |
| Advances in Plasma Diagnostics and Applications 专著 Beijing:MDPI, 2022 作者: Editors:Chen ZT; Attri P; Wang Q(汪球) Adobe PDF(20682Kb)  |  收藏  |  浏览/下载:408/1  |  提交时间:2022/12/03 |