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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:174/37  |  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:256/102  |  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:249/48  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| 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 |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247 Authors: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(2818Kb)  |  Favorite  |  View/Download:256/106  |  Submit date:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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:395/103  |  Submit date:2020/11/30 Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8 Authors: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙) Adobe PDF(1961Kb)  |  Favorite  |  View/Download:258/100  |  Submit date:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163 Authors: Wang XJ; Wang RX(王睿星); Wang L; Chen XJ; Geng XY View  |  Adobe PDF(3200Kb)  |  Favorite  |  View/Download:469/103  |  Submit date:2018/10/30 Non-probabilistic reliability based multidisciplinary design optimization Single loop strategy Uncertainty multidisciplinary analysis Non-probabilistic reliability analysis Translating distance calculation |
| Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230 Authors: Chen XJ; Qiu ZP; Wang XJ; Li YL; Wang RX(王睿星) View  |  Adobe PDF(4860Kb)  |  Favorite  |  View/Download:375/83  |  Submit date:2018/02/08 Uncertain Reduced-order Modeling Robust Flutter Analysis Interval Perturbation Method Uncertain Aeroelastic System |