Selected(0)Clear
Items/Page: Sort: |
| 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:334/121  |  Submit date:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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:310/122  |  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)![](/image/person.jpg)
Adobe PDF(2608Kb)  |   Favorite  |  View/Download:283/123  |  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:460/119  |  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)![](/image/person.jpg)
Adobe PDF(5176Kb)  |   Favorite  |  View/Download:301/116  |  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)![](/image/person.jpg)
Adobe PDF(2023Kb)  |   Favorite  |  View/Download:367/113  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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:284/97  |  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:302/114  |  Submit date:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |