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| 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:564/79  |  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:292/83  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184 作者: Teng, Honghui; Zhang, Yuhang; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(1747Kb)  |  收藏  |  浏览/下载:158/31  |  提交时间:2022/07/18 Double wedge Hypersonic flow Initiation structures Oblique detonation Shock interactions |
| A numerical study of oblique detonation re-stabilization by expansion waves 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 8 作者: Yao KP(姚克鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(1789Kb)  |  收藏  |  浏览/下载:205/35  |  提交时间:2022/06/10 Oblique detonation Stationary Thermal choking Expansion waves |
| 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 |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:278/54  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 斜爆轰发动机的推力性能理论分析 期刊论文 力学学报, 2021, 卷号: 53, 期号: 10, 页码: 2853-2864 作者: 杨鹏飞; 张子健; 杨瑞鑫; 滕宏辉; 姜宗林 Adobe PDF(1224Kb)  |  收藏  |  浏览/下载:411/41  |  提交时间:2022/03/16 斜爆轰波 发动机 推力性能 燃烧模式 |
| A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文 16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020 作者: Chen Z(陈阵); Li S(李森); Luo ZT(罗长童); Jiang ZL(姜宗林) Adobe PDF(1545Kb)  |  收藏  |  浏览/下载:145/39  |  提交时间:2021/02/01 |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文 SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2149Kb)  |  收藏  |  浏览/下载:178/51  |  提交时间:2020/12/28 artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |