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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:365/69  |  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 |
| 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:297/85  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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:105/2  |  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:280/55  |  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:416/41  |  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:147/39  |  提交时间:2021/02/01 |
| Numerical investigation of wavelet features in rotating detonations with a two-step induction-reaction model 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4991-5001 作者: Teng HH(滕宏辉); Zhou L; Yang PF(杨鹏飞); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(2507Kb)  |  收藏  |  浏览/下载:288/95  |  提交时间:2020/04/07 Rotating detonation Induction-reaction kinetics Wavelet pattern Oscillations |
| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40 作者: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(4374Kb)  |  收藏  |  浏览/下载:392/137  |  提交时间:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| 宽速域下斜爆轰波加速起爆的数值研究 会议论文 中国力学大会, 中国浙江杭州, 2019年8月25-28日 作者: 韩信; 张子健; 刘云峰; 姜宗林 Adobe PDF(4511Kb)  |  收藏  |  浏览/下载:423/69  |  提交时间:2019/11/21 斜爆轰波 宽速域 加速起爆 斜爆轰发动机 半圆柱型鼓包 数值模拟 |
| Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel 期刊论文 JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381 作者: Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林) Adobe PDF(1208Kb)  |  收藏  |  浏览/下载:621/130  |  提交时间:2018/10/30 copper calorimeter high enthalpy shock tunnel heat transfer hypersonic |