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| Mitigation of Shock-Induced Separation Using Square-Shaped Micro-Serrations-A Preliminary Study 期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 2, 页码: 16
Authors: Yu FY(于方游); Gao ZB(高占彪) ; Zhang QF(张启帆); Yue LJ(岳连捷); Chen H(陈昊)
  Favorite | View/Download：24/0 | Submit date：2024/05/21
micro-serration separation control shock wave/boundary layer interaction |
| Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20
Authors: Tong XT(仝晓通); Yue LJ(岳连捷); Wu WN(邬婉楠); Zhang QF(张启帆); Chen H(陈昊)
Favorite | View/Download：59/0 | Submit date：2024/03/11 |
| Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572
Authors: Tong XT(仝晓通); Yue LJ(岳连捷); Chen H(陈昊); Zhang QF(张启帆); He CM(何成明)
 Adobe PDF(6058Kb) | Favorite | View/Download：183/52 | Submit date：2022/11/28 |
| Interaction of a shock train with inherent isentropic waves in a curved isolator 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 21
Authors: He LH(贺理浩); Chen H(陈昊); Yue LJ(岳连捷); Zhang QF(张启帆); Wu WN(邬婉楠)
Adobe PDF(8942Kb) | Favorite | View/Download：179/54 | Submit date：2022/11/28 |
| 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：165/33 | 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：211/52 | Submit date：2022/03/05 |
| 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：235/46 | Submit date：2022/02/17 |
| Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors: Zhou GX(周功喜); Zhang X(张旭); Li JP(李进平); Zhang XY(张晓源); Zhang SZ(张仕忠); Lin X(林鑫); Li F(李飞); Chen H(陈宏); Yue LJ(岳连捷); Yu XL(余西龙)
Adobe PDF(4108Kb) | Favorite | View/Download：345/54 | Submit date：2021/09/07
High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
| 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：420/78 | 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：224/59 | Submit date：2021/03/30
Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
