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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:53/11  |  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 |
| 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)![](/image/person.jpg)
Adobe PDF(18431Kb)  |   Favorite  |  View/Download:132/23  |  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)![](/image/person.jpg)
Adobe PDF(7258Kb)  |   Favorite  |  View/Download:124/21  |  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![](/image/person.jpg)
Adobe PDF(6797Kb)  |   Favorite  |  View/Download:422/44  |  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 |
| Dynamic shock interaction mechanism of stage separation for a two-stage-to-orbit vehicle in hypersonic flow 会议论文 空天飞行高温气动全国重点实验室(筹)2023年度夏季学术交流会暨高温气动学术前沿专题研讨会, 怀来, 2023-8-27 ~ 2023-8-29 Authors: Wang Y(王粤) ; Wang YP(汪运鹏)![](/image/person.jpg)
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| 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![](/image/person.jpg)
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| Experimental and numerical investigation on the longitudinal stage separation for parallel-stage two-stage-to-orbit vehicle 会议论文 34th International Symposium on Shock Waves, 韩国, 16-21 July, 2023 Authors: Wang Y(王粤) ; Wang YP(汪运鹏) ; Jiang ZL(姜宗林)![](/image/person.jpg)
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| 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![](/image/person.jpg)
![](/themes/default/image/downing1.png) Favorite  |  View/Download:108/0  |  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![](/image/person.jpg)
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| 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)![](/image/person.jpg)
Adobe PDF(9327Kb)  |   Favorite  |  View/Download:233/72  |  Submit date:2023/05/26 Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |