Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
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：348/176  |  Submit date：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
Authors:  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)  |  Favorite  |  View/Download：213/54  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
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：271/101  |  Submit date：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
超高速流动气动热及壁面催化效应试验研究 期刊论文
中国科学:技术科学, 2020, 卷号: 50, 期号: 08, 页码: 1095-1101
Authors:  周凯;  彭俊;  欧东斌;  胡宗民;  姜宗林
View  |  Adobe PDF(3177Kb)  |  Favorite  |  View/Download：238/61  |  Submit date：2020/09/01
超高速  气动加热  膨胀风洞  壁面催化效应  热流率  
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：268/83  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
激波风洞7°尖锥边界层转捩实验研究 期刊论文
北京航空航天大学学报, 2020, 卷号: 46, 期号: 11, 页码: 2087-2093
Authors:  栗继伟;  卢盼;  汪球;  赵伟
Adobe PDF(2050Kb)  |  Favorite  |  View/Download：179/56  |  Submit date：2021/01/29