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| PyVT: A python-based open-source software for visualization and graphic analysis of fluid dynamics datasets 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 9 Authors: Liu, Qing; Qiao, Zheng; Lv Y(吕钰)
Adobe PDF(1876Kb)  |   Favorite  |  View/Download:242/73  |  Submit date:2021/11/01 Visualization VTK PyQt5 Fluid dynamics |
| 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)![](/image/person.jpg)
Adobe PDF(8841Kb)  |   Favorite  |  View/Download:292/109  |  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)![](/image/person.jpg)
Adobe PDF(2954Kb)  |   Favorite  |  View/Download:300/73  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| 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)![](/image/person.jpg)
Adobe PDF(2818Kb)  |   Favorite  |  View/Download:318/120  |  Submit date:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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)![](/image/person.jpg)
Adobe PDF(2023Kb)  |   Favorite  |  View/Download:345/107  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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)![](/image/person.jpg)
Adobe PDF(1858Kb)  |   Favorite  |  View/Download:226/91  |  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:266/93  |  Submit date:2020/07/06 Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| 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)![](/image/person.jpg)
Adobe PDF(1961Kb)  |   Favorite  |  View/Download:294/112  |  Submit date:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| 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)![](/image/person.jpg)
View  |   Adobe PDF(3862Kb)  |   Favorite  |  View/Download:362/127  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342 Authors: Meng BQ(孟宝清); Han GL(韩桂来) ; Luo ZT(罗长童) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(1937Kb)  |   Favorite  |  View/Download:274/89  |  Submit date:2018/10/30 Hypersonic Shock tunnel Start-up process Impulse force Vibration |