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| 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:256/102  |  Submit date:2021/11/01 Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| 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:239/47  |  Submit date:2021/11/01 Store separation Aerodynamic modeling Interference aerodynamics Dynamic simulation Air-launch-to-orbit |
| A sharp interface immersed boundary method for flow-induced noise prediction using acoustic perturbation equations 期刊论文 COMPUTERS & FLUIDS, 2021, 卷号: 227, 页码: 15 Authors: Zhao, Cheng; Yang Y(杨焱); Zhang, Tao; Dong, Haibo; Hou, Guoxiang Adobe PDF(3919Kb)  |  Favorite  |  View/Download:280/65  |  Submit date:2021/08/30 Acoustic perturbation equations Immersed boundary method Flow-induced noise Four-cylinder array |
| Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics 期刊论文 PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11 Authors: Yu JP(于江鹏); Li JP(李进平); Wang Q(汪球); Zhang SZ(张仕忠); Zhang XY(张晓源) Adobe PDF(3271Kb)  |  Favorite  |  View/Download:217/40  |  Submit date:2021/11/01 |
| 基于人工神经网络的物性预测与反应流场重构研究 学位论文 博士论文,北京: 中国科学院大学, 2021 Authors: 李波 Adobe PDF(14001Kb)  |  Favorite  |  View/Download:506/13  |  Submit date:2021/06/02 计算流体力学,人工神经网络,真实气体物性预测,全流场重构,燃烧热释放速率重构 |
| 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:186/41  |  Submit date:2021/06/07 Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner 期刊论文 COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18 Authors: Tong FL(童福林); Li XL(李新亮); Yuan XX; Yu ZP(于长平) Adobe PDF(7909Kb)  |  Favorite  |  View/Download:339/106  |  Submit date:2020/04/07 Shock wave Turbulent boundary layer Unsteadiness Expansion corner |
| Numerical simulation of acoustic scattering and flow-induced noise with sharp interface immersed boundary method 会议论文 AIAA Scitech 2020 Forum, Orlando, FL, 2020/1/6-10 Authors: Zhao C; Yang Y(杨焱); Zhang T; Dong HB Adobe PDF(1785Kb)  |  Favorite  |  View/Download:115/48  |  Submit date:2021/02/01 |
| 超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文 博士论文,北京: 中国科学院大学, 2019 Authors: 孟宇 Adobe PDF(11443Kb)  |  Favorite  |  View/Download:667/44  |  Submit date:2019/11/07 超燃冲压发动机,燃烧模态,火焰结构,加速过程,微波,滑移电弧,等离子体 |
| 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) Adobe PDF(3862Kb)  |  Favorite  |  View/Download:324/112  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |