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| 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
作者: 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) |  收藏 | 浏览/下载：261/107 | 提交时间：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
作者: Zhang W; Wang S; Wang Q; Ju SJ(鞠胜军); Yan C
Adobe PDF(2859Kb) | 收藏 | 浏览/下载：250/97 | 提交时间：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
作者: 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)
Adobe PDF(2608Kb) | 收藏 | 浏览/下载：262/109 | 提交时间：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
作者: Ju SJ(鞠胜军); Sun ZX(孙振旭); Yang GW(杨国伟); Prapamonthon P; Zhang JY
Adobe PDF(3818Kb) | 收藏 | 浏览/下载：407/103 | 提交时间：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
作者: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | 收藏 | 浏览/下载：249/101 | 提交时间：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
作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | 收藏 | 浏览/下载：299/95 | 提交时间：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
作者: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1657Kb) | 收藏 | 浏览/下载：263/90 | 提交时间：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
作者: Yang L(杨磊); Sun QH(孙泉华)
Adobe PDF(1858Kb) | 收藏 | 浏览/下载：212/89 | 提交时间：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
作者: Jin Y; Liao F(廖飞); Cai JS; Morris PJ
Adobe PDF(7457Kb) | 收藏 | 浏览/下载：238/87 | 提交时间：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
作者: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙)
Adobe PDF(1961Kb) | 收藏 | 浏览/下载：263/102 | 提交时间：2020/05/18
Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
