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Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  收藏  |  浏览/下载：297/85  |  提交时间：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
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
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载：270/107  |  提交时间：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
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  
An improved continuity-preserving interface reconstruction method for multi-material flow 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 224, 页码: 13
作者:  Liu, Shengping;  Yong, Heng;  Guo, Shaodong;  Shen YQ(申义庆);  Ni, Guoxi
Adobe PDF(2093Kb)  |  收藏  |  浏览/下载：318/41  |  提交时间：2021/08/03
Dynamic programming interface reconstruction  Continuity-preserving  Volume-preserving  
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：380/62  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
作者:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
Adobe PDF(6207Kb)  |  收藏  |  浏览/下载：242/97  |  提交时间：2021/02/09
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：255/103  |  提交时间：2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
作者:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  收藏  |  浏览/下载：333/227  |  提交时间：2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
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  
Effects of Different Particle Size Distributions on Aluminum Particle-Air Detonation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 7, 页码: 3115-3128
作者:  Zhang ZJ(张子健);  Wen CY;  Liu YF(刘云峰);  Zhang DL(张德良);  Jiang ZL(姜宗林)
Adobe PDF(2342Kb)  |  收藏  |  浏览/下载：269/104  |  提交时间：2020/08/26