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| 背负式两体分离流动机理与安全分离方案研究 学位论文 博士论文,北京: 中国科学院大学, 2024 Authors: 王粤![](/image/person.jpg)
Adobe PDF(35220Kb)  |   Favorite  |  View/Download:27/5  |  Submit date:2024/06/04 两级入轨 级间分离 高超声速 非定常流动 气动干扰 |
| Influence of non-thermal plasma and electric field on non-premixed methane flame 期刊论文 THERMAL SCIENCE AND ENGINEERING PROGRESS, 2024, 卷号: 47, 页码: 15 Authors: Zhang YF(张玉锋) ; Li T(李腾) ; Wei XL(魏小林)![](/image/person.jpg)
![](/themes/default/image/downing1.png) Favorite  |  View/Download:58/0  |  Submit date:2024/03/11 Non -thermal plasma Coaxial micro -tube burner Methane flame Combustion stability |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文 航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126 Authors: 王粤 ; 汪运鹏 ; 姜宗林![](/image/person.jpg)
Adobe PDF(6797Kb)  |   Favorite  |  View/Download:412/43  |  Submit date:2022/12/01 两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| 基于神经网络和Volterra级数的非定常气动力建模方法研究 学位论文 硕士论文,北京: 中国科学院大学, 2023 Authors: 刘佳昕![](/image/person.jpg)
Adobe PDF(8498Kb)  |   Favorite  |  View/Download:90/3  |  Submit date:2023/06/25 非定常气动力建模 数据增强 神经网络 Volterra级数 数值模拟 |
| 机体尾缘形状对高压捕获翼构型亚声速特性影响 期刊论文 航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215 Authors: 王浩祥; 肖尧; 张凯凯 ; 李广利 ; 常思源 ; 田中伟; 崔凯![](/image/person.jpg)
Adobe PDF(2111Kb)  |   Favorite  |  View/Download:192/52  |  Submit date:2022/10/17 高压捕获翼 亚声速 流动特性 流动分离 数值模拟 |
| 一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文 航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634 Authors: 王粤 ; 汪运鹏 ; 王春 ; 姜宗林![](/image/person.jpg)
Adobe PDF(4901Kb)  |   Favorite  |  View/Download:613/93  |  Submit date:2022/07/11 两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| 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:431/82  |  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:340/100  |  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:336/93  |  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:496/17  |  Submit date:2023/02/06 软件,湍流,高超声速,直接数值模拟,图形处理器 |