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| Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation 期刊论文 Acta Astronautica, 2024, 卷号: 216, 页码: 488-503 Authors: Wang Y(王粤); Wang YP(汪运鹏) Adobe PDF(18431Kb)  |  Favorite  |  View/Download:68/10  |  Submit date:2024/01/18 Multibody separation Hypersonic Dynamic stability Center of pressure Aerodynamic interaction Numerical simulation |
| Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文 Physics of Fluids, 2024, 卷号: 36, 页码: 016116 Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(7258Kb)  |  Favorite  |  View/Download:57/10  |  Submit date:2024/01/15 Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| 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 Adobe PDF(6797Kb)  |  Favorite  |  View/Download:321/32  |  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 |
| 一种用于激波风洞动态试验的时间标定方法及装置 专利 发明专利. 一种用于激波风洞动态试验的时间标定方法及装置, 专利号: CN202210553749.3, 申请日期: 2022-05-20, 授权日期: 2023-07-21 Inventors: 汪运鹏; 王粤; 姜宗林 Adobe PDF(2301Kb)  |  Favorite  |  View/Download:20/2  |  Submit date:2024/01/23 |
| 基于高速气动弹射技术的激波风洞模拟试验装置及方法 专利 发明专利. 基于高速气动弹射技术的激波风洞模拟试验装置及方法, 专利号: 2022105537506, Inventors: 汪运鹏; 王粤; 姜宗林 Favorite  |  View/Download:69/0  |  Submit date:2023/08/28 |
| 基于高速气动弹射技术的激波风洞模拟试验装置及方法 专利 发明专利. 基于高速气动弹射技术的激波风洞模拟试验装置及方法, 专利号: CN202210553750.6, 申请日期: 2022-05-20, 授权日期: 2023-06-23 Inventors: 汪运鹏; 王粤; 姜宗林 Adobe PDF(1349Kb)  |  Favorite  |  View/Download:41/3  |  Submit date:2024/01/23 |
| Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120 Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9327Kb)  |  Favorite  |  View/Download:177/56  |  Submit date:2023/05/26 Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
| 一种非定常压力和气动力数据风洞试验结果处理方法 专利 发明专利. 一种非定常压力和气动力数据风洞试验结果处理方法, 专利号: 2022106077919, 申请日期: 2022-05-31, 授权日期: 2023-03-21 Inventors: 汪运鹏; 王粤; 姜宗林 Adobe PDF(605Kb)  |  Favorite  |  View/Download:53/15  |  Submit date:2023/08/18 |
| 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) Adobe PDF(5479Kb)  |  Favorite  |  View/Download:350/65  |  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 |
| 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 Adobe PDF(4901Kb)  |  Favorite  |  View/Download:538/78  |  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 |