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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:227/51  |  Submit date:2022/06/11 Detached-eddy simulation Reynolds-stress model Massively separated flows Tandem cylinders Launch vehicle Transonic buffet |
| Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21 Authors: Yang L(杨磊); Ye, Zhengyin; Li WH(李文皓); Sun QH(孙泉华) Adobe PDF(4621Kb)  |  Favorite  |  View/Download:290/64  |  Submit date:2021/11/01 Store separation Aerodynamic modeling Interference aerodynamics Dynamic simulation Air-launch-to-orbit |
| Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788 Authors: Xue, Rui; Zheng, Xing; Yue LJ(岳连捷); Zhang, Qian; He, Xin; Yang, Jing; Weng, Chao; Li, Zhihao Adobe PDF(5483Kb)  |  Favorite  |  View/Download:160/48  |  Submit date:2022/10/25 Boundary layer combustion Skin-friction reduction Supersonic combustion Scramjet engine |
| 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 |
| 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:295/118  |  Submit date:2021/02/09 Aerodynamic thermal Opposing jets Parametric sensitivity analysis Uncertainty quantification Analysis of Variance Non-Intrusive Polynomial Chaos |
| 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:447/115  |  Submit date:2020/11/30 Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8 Authors: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(1657Kb)  |  Favorite  |  View/Download:286/101  |  Submit date:2020/08/26 Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| A multi-time scale solution strategy for an elastomeric aircraft 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13 Authors: Yang L(杨磊); Sun QH(孙泉华) Adobe PDF(1858Kb)  |  Favorite  |  View/Download:227/91  |  Submit date:2020/08/26 Flight dynamic simulation Multi-time scale Elastomeric aircraft Reduced order models Store separation |
| Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22 Authors: Jin Y; Liao F(廖飞); Cai JS; Morris PJ Adobe PDF(7457Kb)  |  Favorite  |  View/Download:267/93  |  Submit date:2020/07/06 Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9 Authors: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮) View  |  Adobe PDF(2894Kb)  |  Favorite  |  View/Download:414/151  |  Submit date:2020/03/21 Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |