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| Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect 期刊论文 PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11 Authors: Yang L(杨理); Yue LJ(岳连捷); Yu, Dehai; Chen, Zheng Adobe PDF(4548Kb)  |  Favorite  |  View/Download:170/44  |  Submit date:2022/12/29 |
| Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文 AIAA JOURNAL, 2022, 页码: 9 Authors: Wu ZJ(吴振杰); Zhang QF(张启帆); Zhang X(张旭); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷) Adobe PDF(3049Kb)  |  Favorite  |  View/Download:164/24  |  Submit date:2022/07/18 |
| Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文 AIAA JOURNAL, 2022, 页码: 7 Authors: Zhang X(张旭); Zhang QF(张启帆); Wu ZJ(吴振杰); Yue LJ(岳连捷); Gao ZB(高占彪); Luo WH(罗苇航); Chen H(陈昊) Adobe PDF(1382Kb)  |  Favorite  |  View/Download:157/27  |  Submit date:2022/03/22 |
| Onset of Oblique Detonation Waves for a Cavity-Based Wedge 期刊论文 AIAA JOURNAL, 2022, 页码: 14 Authors: Yang, Li; Yue LJ(岳连捷); Zhang QF(张启帆) Adobe PDF(5573Kb)  |  Favorite  |  View/Download:197/46  |  Submit date:2022/03/05 |
| 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:225/49  |  Submit date:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文 AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882 Authors: Huang TL(黄庭隆); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang P; Zhao QJ Adobe PDF(2961Kb)  |  Favorite  |  View/Download:224/44  |  Submit date:2022/02/17 |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22 Authors: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(8067Kb)  |  Favorite  |  View/Download:403/71  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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:212/53  |  Submit date:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13 Authors: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇) Adobe PDF(5176Kb)  |  Favorite  |  View/Download:279/113  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10 Authors: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇) View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download:355/125  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |