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Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
作者:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  收藏  |  浏览/下载：218/32  |  提交时间：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
Experimental and numerical investigations into flow features in an intake duct for the waterjet propulsion under mooring conditions 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 18
作者:  Huang RF(黄仁芳);  Zhang, Ruizhi;  Wang YW(王一伟);  Luo, Xianwu;  Zhu, Lei
Adobe PDF(11187Kb)  |  收藏  |  浏览/下载：224/44  |  提交时间：2021/06/21
Waterjet propulsion  Particle image velocimetry (PIV)  Intake duct  Waterjet pump  Mooring conditions  
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  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载：278/54  |  提交时间：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
作者:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  收藏  |  浏览/下载：380/57  |  提交时间：2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
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：188/45  |  提交时间：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(4075Kb)  |  收藏  |  浏览/下载：293/85  |  提交时间：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
A nonlinear model for aerodynamic configuration of wake behind horizontal-axis wind turbine 期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2019, 卷号: 40, 期号: 9, 页码: 1313-1326
作者:  Li DS;  Guo T;  Li RN;  Yang CX;  Cheng ZX;  Li Y;  Hu WR(胡文瑞)
浏览  |  Adobe PDF(1504Kb)  |  收藏  |  浏览/下载：170/72  |  提交时间：2019/10/21
nonlinear wake aerodynamic model  vortex-induced velocity  integral equation of vortex-induced velocity  horizontal-axis wind turbine  O355  
Constrained Brownian Motion of a Single Ellipsoid in a Narrow Channel 期刊论文
CHINESE PHYSICS LETTERS, 2019, 卷号: 36, 期号: 3, 页码: 4
作者:  Li HH(李瀚海);  Zheng ZY(郑中玉);  Wang YR(王育人)
浏览  |  Adobe PDF(8315Kb)  |  收藏  |  浏览/下载：232/74  |  提交时间：2019/04/11