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| IDDES method based on differential Reynolds-stress model and its application in bluff body turbulent flows 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 119, 页码: 13 Authors: Wang, Gang; Li, Quanzheng; Liu Y(刘毅) Adobe PDF(4661Kb)  |  Favorite  |  View/Download:239/54  |  Submit date:2022/06/11 Detached-eddy simulation Reynolds-stress model Massively separated flows Tandem cylinders Launch vehicle Transonic buffet |
| Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27 Authors: Li, Mengzhe; Wang, Zhikai; Xu, Rongguang; Zhang, Xiaoliang; Chen, Zhitong; Wang Q(汪球) Adobe PDF(8841Kb)  |  Favorite  |  View/Download:301/111  |  Submit date:2021/11/01 Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14 Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬) Adobe PDF(2954Kb)  |  Favorite  |  View/Download:310/77  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9 Authors: Wang KL(王宽亮); Yang PF(杨鹏飞); Teng HH(滕宏辉) Adobe PDF(2853Kb)  |  Favorite  |  View/Download:273/78  |  Submit date:2021/05/17 Oblique detonation Wave complex Instability Thermal choking Expansion corner |
| 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:427/82  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260 Authors: Zhang W; Wang S; Wang Q; Ju SJ(鞠胜军); Yan C Adobe PDF(2859Kb)  |  Favorite  |  View/Download:307/122  |  Submit date:2021/02/09 Aerodynamic thermal Opposing jets Parametric sensitivity analysis Uncertainty quantification Analysis of Variance Non-Intrusive Polynomial Chaos |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9 Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(2608Kb)  |  Favorite  |  View/Download:282/123  |  Submit date:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10 Authors: Ju SJ(鞠胜军); Sun ZX(孙振旭); Yang GW(杨国伟); Prapamonthon P; Zhang JY Adobe PDF(3818Kb)  |  Favorite  |  View/Download:459/119  |  Submit date:2020/11/30 Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| 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:299/116  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8 Authors: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟) Adobe PDF(2023Kb)  |  Favorite  |  View/Download:366/113  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |