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| 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:151/34  |  提交时间:2023/02/07 Symbolic regression machine learning divide and conquer bi-correlation test mathematical modeling genetic programming |
| A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62 作者: Zhang, Zijian; Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(3178Kb)  |  收藏  |  浏览/下载:208/46  |  提交时间:2022/07/18 Chemical equilibrium Detonation Dissociated air Shock relation Theoretical solution |
| Numerical investigation on the generation mechanism of aero-heating of rudder shaft from three-dimensional flow separation and vortices 期刊论文 AIP ADVANCES, 2022, 卷号: 12, 期号: 4, 页码: 13 作者: Lin MY(林明月); Yang F(杨帆); Wang C(王春) Adobe PDF(16512Kb)  |  收藏  |  浏览/下载:152/24  |  提交时间:2022/07/18 |
| Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文 AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17 作者: Zhang WS(张文硕); Zhang, Zijian; Jiang ZL(姜宗林); Han X(韩信); Liu, Yunfeng; Wang, Chun Adobe PDF(15045Kb)  |  收藏  |  浏览/下载:232/22  |  提交时间:2022/01/24 |
| 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:293/49  |  提交时间:2022/01/12 |
| Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文 SHOCK WAVES, 2021, 页码: 8 作者: Wang Q(汪球); Li JP(李进平); Luo K(罗凯); Li JW(栗继伟); Zhao W(赵伟) Adobe PDF(1158Kb)  |  收藏  |  浏览/下载:233/48  |  提交时间:2021/05/17 Hypersonic Aerodynamic heating Detached bow shock Shock tube expansion tube |
| 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:275/52  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:374/56  |  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:323/88  |  提交时间:2021/03/03 Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:313/165  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |