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| 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 作者: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  收藏  |  浏览/下载:346/35  |  提交时间: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 作者: Nie SJ(聂少军); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2346Kb)  |  收藏  |  浏览/下载:21/2  |  提交时间:2024/02/26 Convolutional neural net-works Deep learning Frequency domain analysis Force measurement Time domain analysis Recurrent neural networks |
| 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 |
| 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 作者: 王粤; 汪运鹏; 王春; 姜宗林 Adobe PDF(4901Kb)  |  收藏  |  浏览/下载:565/79  |  提交时间: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 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 |
| 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 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2434Kb)  |  收藏  |  浏览/下载:305/81  |  提交时间: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 |
| An experimental study of formation of stabilized oblique detonation waves in a combustor 期刊论文 COMBUSTION AND FLAME, 2022, 卷号: 237, 页码: 5 作者: Zhang ZJ(张子健); Wen, Chihyung; Yuan CK(苑朝凯); Liu YF(刘云峰); Han GL(韩桂来); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(865Kb)  |  收藏  |  浏览/下载:319/44  |  提交时间:2022/02/17 |
| TSTO马赫7安全级间分离问题的数值研究 期刊论文 力学学报, 2022, 卷号: 54, 期号: 2, 页码: 526-542 作者: 王粤; 汪运鹏; 薛晓鹏; 姜宗林 Adobe PDF(3565Kb)  |  收藏  |  浏览/下载:343/70  |  提交时间:2021/12/23 两级入轨 高超声速 分离流动 气动干扰 级间分离 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 作者: Jiang ZL(姜宗林); Teng, Honghui Adobe PDF(13641Kb)  |  收藏  |  浏览/下载:104/2  |  提交时间:2023/03/23 |
| Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2554Kb)  |  收藏  |  浏览/下载:140/27  |  提交时间:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |