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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 |
| 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 |
| Divide and Conquer: A Quick Scheme for Symbolic Regression 期刊论文 INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2022, 卷号: 19, 期号: 08, 页码: 25 作者: Luo ZT(罗长童); Chen C(陈辰); Jiang ZL(姜宗林) Adobe PDF(204Kb)  |  收藏  |  浏览/下载:154/34  |  提交时间:2023/02/07 Symbolic regression machine learning divide and conquer bi-correlation test mathematical modeling genetic programming |
| 高超声速高焓条件下的内嵌式温敏漆测量方法 期刊论文 力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58 作者: 苑朝凯; 姜宗林 Adobe PDF(1381Kb)  |  收藏  |  浏览/下载:126/28  |  提交时间:2022/03/16 温敏漆 热流密度场 辐射效应 高超声速流动 辨识方法 |
| 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 |
| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 作者: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林) Adobe PDF(4805Kb)  |  收藏  |  浏览/下载:302/53  |  提交时间:2022/01/12 |
| 一维与二维爆轰传播的时空关联特性数值研究 期刊论文 力学学报, 2021, 卷号: 53, 期号: 07, 页码: 2069-2078 作者: 张文硕; 杨鹏飞; 姜宗林; 刘云峰 Adobe PDF(1701Kb)  |  收藏  |  浏览/下载:199/47  |  提交时间:2021/08/25 斜爆轰 活塞 时空关联 基元反应模型 |
| Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 7 作者: Peng, Di; Liu, Xu; Jiao, Lingrui; Li, Ziyan; Wen, Xin; Yuan CK(苑朝凯); Han GL(韩桂来); Liu YF(刘云峰); Liu, Yingzheng; Jiang ZL(姜宗林) Adobe PDF(3477Kb)  |  收藏  |  浏览/下载:247/47  |  提交时间:2021/03/30 Temperature-sensitive paint Time-resolved measurement Hypersonic flow Background radiation |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 作者: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  收藏  |  浏览/下载:380/57  |  提交时间:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文 COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436 作者: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(3599Kb)  |  收藏  |  浏览/下载:327/89  |  提交时间:2021/03/03 Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |