IMECH-IR

Browse/Search Results:  1-10 of 31 Help

Filters    
Selected(0)Clear Items/Page:    Sort:
Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu YF(刘云峰);  Wang C(王春)
Adobe PDF(15045Kb)  |  Favorite  |  View/Download:275/31  |  Submit date:2022/01/24
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV 期刊论文
Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1
Authors:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平);  Tong FL(童福林)
Adobe PDF(4454Kb)  |  Favorite  |  View/Download:297/44  |  Submit date:2021/11/01
Lifting body model  Hypersonic transition  Direct numerical simulation  
Numerical study on aerodynamic performance of waverider with a new bluntness method 期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
Authors:  Qu ZP;  Xiao HD;  Lv MY;  Li GL(李广利);  Cui K(崔凯)
Adobe PDF(1179Kb)  |  Favorite  |  View/Download:267/110  |  Submit date:2021/06/11
bluntness method  computational fluid dynamics  hypersonic  volume  Waverider  
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone 期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
Adobe PDF(11175Kb)  |  Favorite  |  View/Download:367/104  |  Submit date:2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
The mechanical behavior and collapse of graphene-assembled hollow nanospheres under compression 期刊论文
CARBON, 2021, 卷号: 173, 页码: 600-608
Authors:  Zhao, Yifan;  Zhao, Yushun;  Wu, Fan;  Zhao, Yue;  Wang, Yaming;  Sui, Chao;  He, Xiaodong;  Wang C(王超);  Tan, Huifeng;  Wang, Chao
Adobe PDF(3740Kb)  |  Favorite  |  View/Download:321/60  |  Submit date:2021/04/19
Graphene  Hollow nanosphere  In-situ test  Compressive mechanical properties  
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
Authors:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  Favorite  |  View/Download:360/240  |  Submit date:2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method 期刊论文
Aerospace Science and Technology, 2018, 卷号: 75, 页码: 200-214
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Wang FM(王发民)
View  |  Adobe PDF(2721Kb)  |  Favorite  |  View/Download:609/138  |  Submit date:2018/06/16
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download:403/107  |  Submit date:2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
A modified multi-objective sorting particle swarm optimization and its application to the design of the nose shape of a high-speed train 期刊论文
ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2015, 卷号: 9, 期号: 1, 页码: 513-527
Authors:  Yao SB(姚栓宝);  Guo DL(郭迪龙);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Sun, ZX
View  |  Adobe PDF(1629Kb)  |  Favorite  |  View/Download:322/92  |  Submit date:2018/07/06
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods 期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
Adobe PDF(1133Kb)  |  Favorite  |  View/Download:985/266  |  Submit date:2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference