Elastic postbuckling response of axially-loaded cylindrical shells with seeded geometric imperfection design

被引:22
作者
Hu, Nan [1 ]
Burgueno, Rigoberto [1 ]
机构
[1] Michigan State Univ, Dept Civil & Environm Engn, E Lansing, MI 48824 USA
基金
美国国家科学基金会;
关键词
Postbuckling; Cylindrical shells; Geometric Imperfections; Experiment; 3D Printing; KNOCK-DOWN FACTORS; BUCKLING ANALYSIS; BEHAVIOR; STABILITY; PRESSURE;
D O I
10.1016/j.tws.2015.08.014
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Elastic instabilities (such as buckling) have been recognized as a promising phenomenon to design smart materials and mechanical systems. Thin-walled cylindrical shells under axial compression can attain multiple bifurcation points in their postbuckling regime due to the natural transverse deformation restraint provided by their geometry; but harnessing such behavior for smart purposes is lacking extensive study due to its notoriously high imperfection sensitivity. In this paper, the concept of seeded geometric imperfection (SGI) design is proposed to modify and control the elastic postbuckling behavior of cylindrical shells. Eigenvalue-based mode shapes were used as basic geometric forms to generate a seeded imperfection. Prototyped SGI cylindrical shells were fabricated through 3D printing and tested under loading-unloading cycles. Numerical and experimental results suggest that the SGI cylindrical shells are less sensitive to initial imperfections and load variation than uniform ones. Cylindrical shells with seeded geometry can be potentially used in the design of smart devices and mechanical systems such as energy harvesters and self-powered sensors. (c) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:256 / 268
页数:13
相关论文
共 62 条
[1]  
[Anonymous], 2012, ABAQUS US MAN VERS 6
[2]  
[Anonymous], 2013, 54 AIAA ASME ASCE AH
[3]  
Bazant ZP, 2000, Z ANGEW MATH MECH, V80, P709, DOI 10.1002/1521-4001(200011)80:11/12<709::AID-ZAMM709>3.0.CO
[4]  
2-9
[5]   An experimental investigation into the buckling and post-buckling of CFRP shells under combined axial and torsion loading [J].
Bisagni, C ;
Cordisco, P .
COMPOSITE STRUCTURES, 2003, 60 (04) :391-402
[6]   Numerical analysis and experimental correlation of composite shell buckling and post-buckling [J].
Bisagni, C .
COMPOSITES PART B-ENGINEERING, 2000, 31 (08) :655-667
[7]   Semi-flexible bimetal-based thermal energy harvesters [J].
Boisseau, S. ;
Despesse, G. ;
Monfray, S. ;
Puscasu, O. ;
Skotnicki, T. .
SMART MATERIALS AND STRUCTURES, 2013, 22 (02)
[8]   Efficient modeling of imperfections for buckling analysis of composite cylindrical shells [J].
Broggi, M. ;
Schueller, G. I. .
ENGINEERING STRUCTURES, 2011, 33 (05) :1796-1806
[9]   Tailoring the elastic postbuckling response of thin-walled cylindrical composite shells under axial compression [J].
Burgueno, Rigoberto ;
Hu, Nan ;
Heeringa, Annelise ;
Lajnef, Nizar .
THIN-WALLED STRUCTURES, 2014, 84 :14-25
[10]   Geometric imperfections and lower-bound methods used to calculate knock-down factors for axially compressed composite cylindrical shells [J].
Castro, Saullo G. P. ;
Zimmermann, Rolf ;
Arbelo, Mariano A. ;
Khakimova, Regina ;
Hilburger, Mark W. ;
Degenhardt, Richard .
THIN-WALLED STRUCTURES, 2014, 74 :118-132