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| 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 Authors: Zhang, Zijian; Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(3178Kb)  |  Favorite  |  View/Download:266/62  |  Submit date:2022/07/18 Chemical equilibrium Detonation Dissociated air Shock relation Theoretical solution |
| 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 Authors: Zhang WS(张文硕); Zhang, Zijian; Jiang ZL(姜宗林); Han X(韩信); Liu YF(刘云峰); Wang C(王春) Adobe PDF(15045Kb)  |  Favorite  |  View/Download:282/32  |  Submit date:2022/01/24 |
| 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:296/67  |  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:311/70  |  Submit date: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 Authors: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  Favorite  |  View/Download:437/79  |  Submit date:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| 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 Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  Favorite  |  View/Download:363/179  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  Favorite  |  View/Download:288/102  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| 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 Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林) View  |  Adobe PDF(4374Kb)  |  Favorite  |  View/Download:443/154  |  Submit date:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306 Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林) View  |  Adobe PDF(2165Kb)  |  Favorite  |  View/Download:432/100  |  Submit date:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |