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| Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16 作者: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利); Tian ZW(田中伟); Cui K(崔凯) 收藏  |  浏览/下载:67/0  |  提交时间:2024/01/22 High-pressure capturing wing Subsonic Numerical simulation Wing dihedral Stability |
| Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18 作者: Guo SQ(郭帅旗); Liu W(刘文); Zhang CA(张陈安); Liu Y(刘洋); Wang FM(王发民) 收藏  |  浏览/下载:23/0  |  提交时间:2024/02/05 Hypersonic waverider Aerodynamic model Symbolic regression Bluntness effect |
| Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15 作者: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利); Tian ZW(田中伟); Cui K(崔凯) Adobe PDF(8136Kb)  |  收藏  |  浏览/下载:40/2  |  提交时间:2024/03/11 High-pressure capturing wing Hypersonic Numerical simulation Wing dihedral Stability |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22 作者: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(8067Kb)  |  收藏  |  浏览/下载:378/62  |  提交时间:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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:263/108  |  提交时间: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 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:411/103  |  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:254/103  |  提交时间:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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:241/87  |  提交时间:2020/07/06 Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇) 浏览  |  Adobe PDF(3918Kb)  |  收藏  |  浏览/下载:521/165  |  提交时间:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306 作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(2165Kb)  |  收藏  |  浏览/下载:396/92  |  提交时间:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |