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| Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文
AIAA JOURNAL, 2024, 页码: 8
Authors: Wang WT(王文韬) ; Wang Q(汪球); Li JP(李进平); Zhao W(赵伟); Gao, Liangjie; Liu, Zhongchen; Qian, Zhansen
  Favorite | View/Download：60/0 | Submit date：2024/02/26
Finite Element Method Hypersonic Shock Tube/Tunnel Diaphragm Burst Pressure |
| 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：92/18 | Submit date：2024/01/15
Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
Authors: Yao KP(姚克鹏); Yang PF(杨鹏飞); Wang C(王春); Jiang ZL(姜宗林)
Adobe PDF(8005Kb) | Favorite | View/Download：39/4 | Submit date：2024/02/19 |
| 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：381/39 | 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 |
| Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
Authors: Nie SJ(聂少军); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2346Kb) | Favorite | View/Download：55/11 | Submit date：2024/02/26
Convolutional neural net-works Deep learning Frequency domain analysis Force measurement Time domain analysis Recurrent neural networks |
| 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：53/13 | Submit date：2024/01/23 |
| 激波风洞测力信号的频域数据深度学习建模分析方法 期刊论文
振动与冲击, 2023, 卷号: 42, 期号: 13, 页码: 296-302+315
Authors: 聂少军; 汪运鹏; 王春; 姜宗林
Adobe PDF(665Kb) | Favorite | View/Download：195/50 | Submit date：2023/08/02
激波风洞 气动力测量 惯性振动 深度学习 频域分析 |
| 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：81/0 | 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：82/16 | 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：209/67 | Submit date：2023/05/26
Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
