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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Numerical Investigation of the Influence of Fuselage Corner Bluntness on a High-Pressure Capturing Wing Configuration
期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2025, 卷号: 38, 期号: 2, 页码: 13./通讯作者:Li, Guangli
Authors:
Xi XZ(席小喆)
;
Li GL(李广利)
;
Wang HX(王浩祥)
;
Xiao, Yao
;
Chang SY(常思源)
;
Cui K(崔凯)
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View/Download:215/0
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Submit date:2025/02/24
High-pressure capturing wing (HCW)
Flow separation
Numerical simulation
Fuselage corner bluntness
Aerodynamic performance
Moisture adsorption-desorption full cycle power generation
期刊论文
NATURE COMMUNICATIONS, 2022, 卷号: 13, 期号: 1, 页码: 11./通讯作者:Liu, Feng, Cheng, Huhu, Qu, Liangti
Authors:
Wang HY
;
He TC
;
Hao XZ
;
Huang YX
;
Yao HZ
;
Liu F(刘峰)
;
Cheng HH
;
Qu LT
Adobe PDF(4548Kb)
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View/Download:334/90
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Submit date:2022/07/18
Experimental and numerical study of circular, stainless thin tube energy absorber under axial impact by a control rod
期刊论文
Thin-Walled Structures, 2014, 卷号: 82, 页码: 24-32
Authors:
Yang Z(杨哲)
;
Yan H
;
Huang CG(黄晨光)
;
Diao XZ
;
Wu XQ(吴先前)
;
Wang SH
;
Lu LL(路玲玲)
;
Liao LJ(廖丽涓)
;
Wei YP(魏延鹏)
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Adobe PDF(2962Kb)
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View/Download:1368/284
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Submit date:2014/09/03
Circular Thin Tube
Energy Absorber
Progressive Buckling
Axial Impact
Strain Rate
Interfacial Pressure
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