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Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  Favorite  |  View/Download：277/60  |  Submit date：2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit  
A multi-time scale solution strategy for an elastomeric aircraft 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13
Authors:  Yang L(杨磊);  Sun QH(孙泉华)
Adobe PDF(1858Kb)  |  Favorite  |  View/Download：221/90  |  Submit date：2020/08/26
Flight dynamic simulation  Multi-time scale  Elastomeric aircraft  Reduced order models  Store separation  
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  Favorite  |  View/Download：281/107  |  Submit date：2020/05/18
Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
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：412/94  |  Submit date：2019/09/09
Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow  
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:  Li HX(李慧鑫);  Ye L(叶亮);  Wei XL(魏小林);  Li T(李腾);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(1708Kb)  |  Favorite  |  View/Download：476/210  |  Submit date：2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance