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| Standing oblique detonation for hypersonic propulsion: A review 期刊论文 PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17 Authors: Jiang ZL(姜宗林) Adobe PDF(10386Kb)  |  Favorite  |  View/Download:66/8  |  Submit date:2024/02/26 Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion |
| Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文 NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19 Authors: Qi L(齐力); Han GL(韩桂来); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(3726Kb)  |  Favorite  |  View/Download:294/64  |  Submit date:2022/07/18 Coaxial thermocouples lateral heat transfer maximum temperature point numerical simulation surface heat flux |
| 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 Authors: Lin MY(林明月); Yang F(杨帆); Wang C(王春) Adobe PDF(16512Kb)  |  Favorite  |  View/Download:191/28  |  Submit date:2022/07/18 |
| 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:343/65  |  Submit date:2022/01/12 |
| 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:356/178  |  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:278/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Numerical simulation of the interaction of two shear layers in double backward-facing steps 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15 Authors: Deng F(邓放); Han GL(韩桂来); Liu MK(刘美宽); Ding, J; Weng, PF; Jiang ZL(姜宗林) View  |  Adobe PDF(5760Kb)  |  Favorite  |  View/Download:561/91  |  Submit date:2019/10/21 |