IMECH-IR

Browse/Search Results:  1-10 of 27 Help

Filters        
Selected(0)Clear Items/Page:    Sort:
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
Authors:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
Adobe PDF(4402Kb)  |  Favorite  |  View/Download:220/53  |  Submit date: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
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download:351/177  |  Submit date:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  Favorite  |  View/Download:273/101  |  Submit date:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
PIMOL: A New Semi-analytical Method Based on the Finite Difference Method of Lines and the Precise Integration Method 期刊论文
ACTA MECHANICA SOLIDA SINICA, 2020, 卷号: 33, 期号: 3, 页码: 381-391
Authors:  Xu YJ(徐永君)
View  |  Adobe PDF(422Kb)  |  Favorite  |  View/Download:253/61  |  Submit date:2020/03/21
PIMOL  ODE  FDMOL  PIM  Poisson's equation  Semi-analytical  Semi-discrete  
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2057Kb)  |  Favorite  |  View/Download:270/83  |  Submit date:2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
PIMOL: The Finite Difference Method of Lines Based on the Precise Integration Method for an Arbitrary Irregular Domain 期刊论文
ACTA MECHANICA SOLIDA SINICA, 2020, 页码: 13
Authors:  Xu YJ(徐永君)
Adobe PDF(704Kb)  |  Favorite  |  View/Download:220/48  |  Submit date:2020/05/18
PIMOL  ODEs  FDMOL  PIM  Poisson's equation problems  Semi-analytical (discrete)  Irregular domain  
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:  Yao W(姚卫)
View  |  Adobe PDF(9586Kb)  |  Favorite  |  View/Download:663/297  |  Submit date:2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Dynamic deformation behavior of a face-centered cubic FeCoNiCrMn high-entropy alloy 期刊论文
Science Bulletin, 2018, 卷号: 63, 期号: 6, 页码: 362-368
Authors:  He JY;  Wang Q;  Zhang HS(张虎生);  Dai LH(戴兰宏);  Mukai T;  Wu Y;  Liu XJ;  Wang H;  Nieh TG;  Lu ZP
View  |  Adobe PDF(3368Kb)  |  Favorite  |  View/Download:536/170  |  Submit date:2018/10/24
High-entropy Alloys  Dynamic Deformation  Deformation Twinning  Work-hardening  Plastic Stability  
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
Authors:  Huang CD(黄程德);  Liu W(刘文);  Yang GW(杨国伟)
View  |  Adobe PDF(4021Kb)  |  Favorite  |  View/Download:342/100  |  Submit date:2017/11/29
Aeroelasticity  Fluid-structure Interpolation  Grid Fin  Mesh Deformation  Radial Basis Function  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1654Kb)  |  Favorite  |  View/Download:373/93  |  Submit date:2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution