Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 13 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
风洞模拟等离子体绕流场回波频谱调制特性实验研究 期刊论文
物理学报, 2022, 卷号: 71, 期号: 03, 页码: 221-227
Authors:  满良;  邓浩川;  吴洋;  余西龙;  肖志河
Adobe PDF(2239Kb)  |  Favorite  |  View/Download：142/48  |  Submit date：2022/03/16
等离子体绕流场  频谱调制  一维距离像  风洞  
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
Authors:  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)  |  Favorite  |  View/Download：300/67  |  Submit date：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
Authors:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  Favorite  |  View/Download：429/76  |  Submit date：2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
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：231/62  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
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：682/302  |  Submit date：2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
Adobe PDF(1468Kb)  |  Favorite  |  View/Download：368/110  |  Submit date：2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel  
Shock oscillation in highly underexpanded jets 期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 9, 页码: 94705
Authors:  Li XP;  Zhou R;  Chen XP;  Fan XJ(范学军);  Xie GS
Adobe PDF(8162Kb)  |  Favorite  |  View/Download：334/95  |  Submit date：2018/10/30
highly underexpanded jets  shock oscillation  large eddy simulation  
Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
Adobe PDF(1161Kb)  |  Favorite  |  View/Download：330/79  |  Submit date：2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
Aerodynamic measurement of a large aircraft model in hypersonic flow 期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Zhang DL(张德良);  Jiang ZL(姜宗林)
Adobe PDF(4916Kb)  |  Favorite  |  View/Download：505/120  |  Submit date：2017/12/18
Hypersonic  Aerodynamic Measurement  Theoretical Study  Vibration  
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.
Adobe PDF(1654Kb)  |  Favorite  |  View/Download：386/98  |  Submit date：2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution