Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters    
Selected(0)Clear Items/Page:    Sort:
Standing oblique detonation for hypersonic propulsion: A review 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
Authors:  Jiang ZL(姜宗林)
Adobe PDF(10386Kb)  |  Favorite  |  View/Download：66/8  |  Submit date：2024/02/26
Standing oblique detonation  Scramjet engine  Oblique detonation engine  Shock wave  Supersonic combustion  Hypersonic ramjet propulsion  
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:  Zhang, Zijian;  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3178Kb)  |  Favorite  |  View/Download：253/60  |  Submit date：2022/07/18
Chemical equilibrium  Detonation  Dissociated air  Shock relation  Theoretical solution  
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：270/31  |  Submit date：2022/01/24
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：295/65  |  Submit date：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
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：357/178  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:  Peng J(彭俊);  Zhang ZJ(张子健);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(2165Kb)  |  Favorite  |  View/Download：424/99  |  Submit date：2019/09/09
Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow