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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:70/0  |  提交时间:2024/01/22
High-pressure capturing wing  Subsonic  Numerical simulation  Wing dihedral  Stability  
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:43/3  |  提交时间:2024/03/11
High-pressure capturing wing  Hypersonic  Numerical simulation  Wing dihedral  Stability  
Development and validation of a combustion large-eddy-simulation solver based on fully compressible formulation and tabulated chemistry 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 127, 页码: 107693
作者:  Zhang HY(张慧颖);  Chen Y(陈与);  Lv Y(吕钰)
Adobe PDF(2375Kb)  |  收藏  |  浏览/下载:90/21  |  提交时间:2022/10/23
Compressible flow  Turbulent combustion  Large-eddy simulation  Non-premixed flame  Flamelet  
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
作者:  Wang, Gang;  Li, Quanzheng;  Liu Y(刘毅)
Adobe PDF(4661Kb)  |  收藏  |  浏览/下载:190/40  |  提交时间:2022/06/11
Detached-eddy simulation  Reynolds-stress model  Massively separated flows  Tandem cylinders  Launch vehicle  Transonic buffet  
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
作者:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  收藏  |  浏览/下载:265/58  |  提交时间: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
作者:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  收藏  |  浏览/下载:257/53  |  提交时间:2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit  
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:256/104  |  提交时间:2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
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:214/89  |  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:242/87  |  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:523/165  |  提交时间:2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation