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Computational study of lateral jet interaction in hypersonic thermochemical non-equilibrium flows using nonlinear coupled constitutive relations 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 11, 页码: 14
作者:  Zeng, Shuhua;  Yang, Junyuan;  Zhao, Wenwen;  Huang YF(黄依峰);  Jiang, Zhongzheng;  Chen, Weifang
Adobe PDF(3990Kb)  |  收藏  |  浏览/下载：61/6  |  提交时间：2024/01/22
Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
作者:  Yang F(杨帆);  Lin MY(林明月);  Hu ZM(胡宗民);  Han GL(韩桂来)
Adobe PDF(8946Kb)  |  收藏  |  浏览/下载：65/2  |  提交时间：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
作者:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  收藏  |  浏览/下载：299/52  |  提交时间：2022/01/12
Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system 期刊论文
NONLINEAR DYNAMICS, 2021, 页码: 22
作者:  Zhu, Hong;  Sun, Qinglin;  Liu, Xuefeng;  Liu, Jinglei;  Sun, Hao;  Wu WN(邬婉楠);  Tan, Panlong;  Chen, Zengqiang
Adobe PDF(4213Kb)  |  收藏  |  浏览/下载：276/47  |  提交时间：2021/08/03
Fluid-structure interaction  Parafoil system  Flexible deformation  Trailing edge deflection  Aerodynamic performance  Dynamic model  
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
作者:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
Adobe PDF(4402Kb)  |  收藏  |  浏览/下载：194/44  |  提交时间：2021/06/07
Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
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：320/168  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
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：236/65  |  提交时间：2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
Characterizing three-dimensional features of vortex surfaces in the flow past a finite plate 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 1, 页码: 15
作者:  Tong WW;  Yang Y(杨越);  Wang SZ(王士召)
Adobe PDF(6216Kb)  |  收藏  |  浏览/下载：251/94  |  提交时间：2020/05/18
External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
作者:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
浏览  |  Adobe PDF(4679Kb)  |  收藏  |  浏览/下载：266/97  |  提交时间：2019/09/09
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
作者:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
浏览  |  Adobe PDF(8635Kb)  |  收藏  |  浏览/下载：211/70  |  提交时间：2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent