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| Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184 Authors: Teng, Honghui; Zhang, Yuhang; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(1747Kb)  |  Favorite  |  View/Download:196/40  |  Submit date:2022/07/18 Double wedge Hypersonic flow Initiation structures Oblique detonation Shock interactions |
| Parameters for evaluating the efficiency of inlet compression 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56 Authors: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(511Kb)  |  Favorite  |  View/Download:229/50  |  Submit date:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文 JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12 Authors: Shi Weixiu; Pan LS(潘利生); Jin Suyi; Dong YH(董跃华); Li T(李腾); Zhao J(赵京); Wei XL(魏小林) Adobe PDF(2198Kb)  |  Favorite  |  View/Download:288/65  |  Submit date:2021/11/01 CO2-based mixture flammability laminar flame speed flammable critical mixing ratio transcritical power cycle |
| 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:293/63  |  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:413/69  |  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:352/177  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH(马生虎); Zhang QF(张启帆); Zhang, Peng; Zhang XY(张新宇) Adobe PDF(3937Kb)  |  Favorite  |  View/Download:217/56  |  Submit date:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| 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:275/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953 Authors: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇) View  |  Adobe PDF(4075Kb)  |  Favorite  |  View/Download:317/95  |  Submit date:2020/03/11 Wall heat flux Numerical simulation Ethylene Supersonic combustor |