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| 风洞模拟等离子体绕流场回波频谱调制特性实验研究 期刊论文 物理学报, 2022, 卷号: 71, 期号: 03, 页码: 221-227 Authors: 满良; 邓浩川; 吴洋; 余西龙; 肖志河 Adobe PDF(2239Kb)  |  Favorite  |  View/Download:134/45  |  Submit date:2022/03/16 等离子体绕流场 频谱调制 一维距离像 风洞 |
| 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:227/49  |  Submit date:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| 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:217/51  |  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:290/61  |  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:407/66  |  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:348/176  |  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:213/54  |  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:271/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475 Authors: Wang Q(汪球); Luo K(罗凯); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟) Adobe PDF(2057Kb)  |  Favorite  |  View/Download:268/83  |  Submit date:2020/08/26 Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |
| Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31 Authors: Yuan CK(苑朝凯); Zhou K(周凯); Liu YF(刘云峰); Hu ZM(胡宗民); Jiang ZL(姜宗林) View  |  Adobe PDF(1468Kb)  |  Favorite  |  View/Download:351/104  |  Submit date:2019/04/11 Spectral measurement Hypervelocity flow Radiation Expansion tunnel |