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| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 Authors: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林) Adobe PDF(4805Kb)  |  Favorite  |  View/Download:327/61  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:270/60  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:290/61  |  Submit date:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文 COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436 Authors: 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)  |  Favorite  |  View/Download:363/92  |  Submit date:2021/03/03 Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |