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| Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文 ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12 Authors: Lin MY(林明月); Yang F(杨帆); Hu ZM(胡宗民); Han GL(韩桂来) Favorite  |  View/Download:25/0  |  Submit date:2024/05/27 Shock waves Shock-shock interaction Theoretical analysis Hysteresis |
| Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363 Authors: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮) Adobe PDF(4402Kb)  |  Favorite  |  View/Download:230/58  |  Submit date:2021/06/07 Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| 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:295/65  |  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:423/75  |  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:357/178  |  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:224/59  |  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:280/102  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface 期刊论文 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3 Authors: Li GL(李广利); Cui K(崔凯); Xu YZ(徐应洲); Wang HX(王浩祥); Yang J(杨靖); Xu XG(许先贵) Adobe PDF(661Kb)  |  Favorite  |  View/Download:424/102  |  Submit date:2020/05/18 |
| 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:322/96  |  Submit date:2020/03/11 Wall heat flux Numerical simulation Ethylene Supersonic combustor |