Energy absorption properties of multi-panel reinforced tubular structure under quasi-static compression loading

被引:1
作者
Wang, Kedi [1 ]
Wang, Han [1 ]
Yang, Huan [2 ]
Wang, Wenzhi [3 ]
Xi, Xulong [2 ]
Bai, Chunyu [2 ]
Bai, Erlei [4 ]
Fan, Xueling [1 ]
机构
[1] Xi An Jiao Tong Univ, Sch Aerosp Engn, Xian Key Lab Extreme Environm & Protect Technol, Xian, Peoples R China
[2] Aircraft Strength Res Inst China, Aviat Key Lab Sci & Technol Struct Impact Dynam, Xian, Peoples R China
[3] Northwestern Polytech Univ, Sch Aeronaut, Xian, Peoples R China
[4] Air Force Engn Univ, Aviat Engn Sch, Xian, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Tubular structure; panel-reinforced; energy absorption; quasi-static compression; TUBES; DESIGN; BAMBOO;
D O I
10.1080/15376494.2024.2443101
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Energy-absorbing structures are widely used in the aerospace and automotive industries. The multi-panel reinforced tubular structure is mainly used in scenarios where size and weight are limited. By adding wall panels to the tubular structure, the energy absorption (EA) properties of the structure can be improved. In this article, the energy absorption properties of convex and concave type panel-reinforced tubular structures are experimentally and numerically studied. The effects of the number and thickness of panels on the energy absorption properties are analyzed. The results show that the convex panel-reinforced tubular structure has better energy absorption properties and a more stable process. The number of panels has little effect on the energy absorption properties of the entire structure. The specific energy absorption of the structure increases with the thickness of panels, but it is expected that there will be an upper limit of about 114 kJ<middle dot>kg-1.
引用
收藏
页数:12
相关论文
共 56 条
[1]   A review on crashworthiness studies of crash box structure [J].
Abdullah, N. A. Z. ;
Sani, M. S. M. ;
Salwani, M. S. ;
Husain, N. A. .
THIN-WALLED STRUCTURES, 2020, 153
[2]   An insight into the quasi-static indentation and specific energy absorption performance of glass fiber-aluminum wire mesh hybrid laminates [J].
Ashry, Mohamed ;
Najjar, I. M. R. ;
Sadoun, A. M. ;
Seif, Amr .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2024,
[3]   Nature-inspired materials and structures using 3D Printing [J].
Bandyopadhyay, Amit ;
Traxel, Kellen D. ;
Bose, Susmita .
MATERIALS SCIENCE & ENGINEERING R-REPORTS, 2021, 145
[4]   Experimental and Numerical Crashworthiness Study of a Full-Scale Composite Fuselage Section [J].
Caputo, F. ;
Lamanna, G. ;
Perfetto, D. ;
Chiariello, A. ;
Di Caprio, F. ;
Di Palma, L. .
AIAA JOURNAL, 2021, 59 (02) :700-718
[5]   Carrera Unified Formulation (CUF) for the composite plates and shells of revolution. Layer-wise models [J].
Carrera, E. ;
Zozulya, V. V. .
COMPOSITE STRUCTURES, 2024, 334
[6]  
Carrera E., 2003, Applied Mechanics Review, V56, P287, DOI 10.1115/1.1557614
[7]   Bending of composites and sandwich plates subjected to localized lateral loadings: a comparison of various theories [J].
Carrera, E ;
Ciuffreda, A .
COMPOSITE STRUCTURES, 2005, 68 (02) :185-202
[8]   Mixed layer-wise models for multilayered plates analysis [J].
Carrera, E .
COMPOSITE STRUCTURES, 1998, 43 (01) :57-70
[9]   Transverse normal stress effects in multilayered plates [J].
Carrera, E .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1999, 66 (04) :1004-1012
[10]  
Carrera E., 2001, Applied Mechanics Reviews, V54, P301