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Study on the propulsive performance of oblique detonation engine 期刊论文
ENERGY, 2024, 卷号: 292, 页码: 11
作者:  Liu YF(刘云峰);  Han, Xin;  Zhang, Zijian
收藏  |  浏览/下载：0/0  |  提交时间：2024/04/15
Oblique detonation engine  ODE  Propulsive performance  Specific impulse  
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文
AIAA JOURNAL, 2024, 页码: 8
作者:  Wang WT(王文韬);  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Gao, Liangjie;  Liu, Zhongchen;  Qian, Zhansen
收藏  |  浏览/下载：39/0  |  提交时间：2024/02/26
Finite Element Method  Hypersonic  Shock Tube/Tunnel  Diaphragm  Burst Pressure  
Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation 期刊论文
Acta Astronautica, 2024, 卷号: 216, 页码: 488-503
作者:  Wang Y(王粤);  Wang YP(汪运鹏)
Adobe PDF(18431Kb)  |  收藏  |  浏览/下载：81/13  |  提交时间：2024/01/18
Multibody separation  Hypersonic  Dynamic stability  Center of pressure  Aerodynamic interaction  Numerical simulation  
Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(7258Kb)  |  收藏  |  浏览/下载：70/15  |  提交时间：2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
Prediction of Transition Locations in Regions of the Minor Axis of Hypersonic Elliptic Cones using the BiGlobal-eN Method 期刊论文
ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2024, 页码: 28
作者:  Zhao, Lei;  Zhou, Wenqiang;  Li XL(李新亮);  Zhang, Shaolong;  Zhang, Yongming
收藏  |  浏览/下载：25/0  |  提交时间：2024/02/19
BiGlobal stability  transition  boundary layer  hypersonic elliptic cone  minor axis.  
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：59/0  |  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：21/0  |  提交时间：2024/02/05
Hypersonic waverider  Aerodynamic model  Symbolic regression  Bluntness effect  
Investigation of high enthalpy thermochemical nonequilibrium flow over spheres 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 10
作者:  Guo, Jinghui;  Wang XY(王小永);  Li, Sijia
收藏  |  浏览/下载：16/0  |  提交时间：2024/02/26
Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20
作者:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Wu WN(邬婉楠);  Zhang QF(张启帆);  Chen H(陈昊)
收藏  |  浏览/下载：16/0  |  提交时间：2024/03/11
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
作者:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
收藏  |  浏览/下载：20/0  |  提交时间：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance