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不同大气条件下超声速降落伞系统气动特性分析 期刊论文
航天返回与遥感, 2020, 卷号: 41, 期号: 06, 页码: 77-89
作者:  姜璐璐;  林明月;  薛晓鹏;  贾贺;  荣伟;  王奇
Adobe PDF(6000Kb)  |  收藏  |  浏览/下载:305/50  |  提交时间:2021/01/29
火星大气  超声速降落伞  气动干扰  数值模拟  火星探测器  
高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
作者:  贺理浩;  张启帆;  岳连捷;  张新宇;  王卫星;  谭慧俊
Adobe PDF(9600Kb)  |  收藏  |  浏览/下载:238/34  |  提交时间:2021/11/12
高速进气道  低马赫数不起动  非定常  气动力  自起动  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:321/168  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  收藏  |  浏览/下载:187/44  |  提交时间:2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020
作者:  Chen Z(陈阵);  Li S(李森);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(1545Kb)  |  收藏  |  浏览/下载:145/39  |  提交时间:2021/02/01
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:253/98  |  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 flow structures resulting from the interaction between an oblique detonation wave and an upper expansion corner 期刊论文
JOURNAL OF FLUID MECHANICS, 2020, 卷号: 903, 页码: 17
作者:  Wang KL(王宽亮);  Teng HH(滕宏辉);  Yang PF(杨鹏飞);  Ng HD
Adobe PDF(1764Kb)  |  收藏  |  浏览/下载:245/67  |  提交时间:2020/11/30
detonation waves  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(1551Kb)  |  收藏  |  浏览/下载:237/66  |  提交时间:2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
Design of a new supersonic biplane 期刊论文
Acta Astronautica, 2020, 卷号: 175, 期号: 10, 页码: 216-233
作者:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW
Adobe PDF(5403Kb)  |  收藏  |  浏览/下载:445/57  |  提交时间:2020/06/08
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