Stability and failure of compressed thin-walled composite columns using experimental tests and advanced numerical damage models

被引:39
作者
Rozylo, Patryk [1 ]
机构
[1] Lublin Univ Technol, Fac Mech Engn, Dept Machine Design & Mechatron, Nadbystrzycka 36, PL-20618 Lublin, Poland
关键词
axial compressive load; buckling and postbuckling; cohesive zone model; experimental tests; finite element method; laminates; progressive failure analysis; INITIAL GEOMETRIC IMPERFECTIONS; CHANNEL-SECTION BEAMS; PROGRESSIVE FAILURE; POSTBUCKLING BEHAVIOR; DEFORMATION STATES; IMPACT DAMAGE; CROSS-SECTION; DELAMINATION; SIMULATION; PROFILES;
D O I
10.1002/nme.6757
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The current study investigates the stability and failure analysis of thin-walled composite columns with a top-hat and channel cross section, subjected to axial compression. The analyzed structures were made of composite material (carbon fiber reinforced polymer) by autoclave technique. The study included experimental tests on actual specimens and numerical simulations on numerical models using finite element method (in ABAQUS (R) program). Experimental-numerical analysis was conducted over the full range of loading (until failure phenomenon). Regarding the experimental tests, postbuckling equilibrium paths as well as acoustic emission signals were registered, which directly allowed for comprehensive analysis of failure phenomenon of composite material. In case of numerical simulations, two independent numerical damage models were used. The first one constitutes the progressive failure analysis, considering the damage initiation criteria using Hashin's theory and damage evolution based on the energy criterion. The second one constitutes the cohesive zone model, which was used to simulate failure of composite material caused by delamination phenomenon. Both experimental and numerical results show high agreement. Furthermore, the obtained results reveal an interesting relationship between buckling, postbuckling, and failure phenomenon of the analyzed structures.
引用
收藏
页码:5076 / 5099
页数:24
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