A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations
A three-dimensional (3D) semi-analytical model is developed by introducing meshfree local radial point interpolation method into a Hamilton system to analyze the mechanical and thermal buckling behavior of rectangular laminated plates with embedded delaminations. A modified Hamiltonian function for...
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2017-11-01
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doaj-f703530c419f4ce09a05edbd9d4ea2d92021-09-05T14:00:31ZengDe GruyterScience and Engineering of Composite Materials0792-12332191-03592017-11-0124693794910.1515/secm-2015-0003A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminationsChen Jie0Wang Hai1Zhang Yingchun2Zhan Lihua3Shanghai Aircraft Airworthiness Certification Center, Civil Aviation Administration of China, 200335 Shanghai, ChinaSchool of Aeronautics and Astronautics, Shanghai Jiao Tong University, 200240 Shanghai, ChinaShanghai Aircraft Airworthiness Certification Center, Civil Aviation Administration of China, 200335 Shanghai, ChinaSchool of Mechanical and Electrical Engineering, Central South University, 410083 Changsha, ChinaA three-dimensional (3D) semi-analytical model is developed by introducing meshfree local radial point interpolation method into a Hamilton system to analyze the mechanical and thermal buckling behavior of rectangular laminated plates with embedded delaminations. A modified Hamiltonian function for mechanical and thermal buckling analysis of rectangular laminated composite plates subjected to in-plane axial compressive or thermal loads is proposed. The final governing equation is deduced with the transfer matrix technique and a spring layer model based on the modified Hellinger-Reissner variational principle. One of the main superiorities of the present model is that the scale of final governing equation, which involves only the so-called state variables at the top and bottom surfaces, is insensitive to the thickness and the number of layers of composite laminates. Several relevant numerical examples are carried out to validate the present model, and the present results are in good agreement with pre-existing results.https://doi.org/10.1515/secm-2015-0003composite laminatedelaminationlocal radial point interpolation methodmechanical bucklingthermal buckling |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Chen Jie Wang Hai Zhang Yingchun Zhan Lihua |
spellingShingle |
Chen Jie Wang Hai Zhang Yingchun Zhan Lihua A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations Science and Engineering of Composite Materials composite laminate delamination local radial point interpolation method mechanical buckling thermal buckling |
author_facet |
Chen Jie Wang Hai Zhang Yingchun Zhan Lihua |
author_sort |
Chen Jie |
title |
A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations |
title_short |
A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations |
title_full |
A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations |
title_fullStr |
A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations |
title_full_unstemmed |
A 3D computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations |
title_sort |
3d computational meshfree model for the mechanical and thermal buckling analysis of rectangular composite laminated plates with embedded delaminations |
publisher |
De Gruyter |
series |
Science and Engineering of Composite Materials |
issn |
0792-1233 2191-0359 |
publishDate |
2017-11-01 |
description |
A three-dimensional (3D) semi-analytical model is developed by introducing meshfree local radial point interpolation method into a Hamilton system to analyze the mechanical and thermal buckling behavior of rectangular laminated plates with embedded delaminations. A modified Hamiltonian function for mechanical and thermal buckling analysis of rectangular laminated composite plates subjected to in-plane axial compressive or thermal loads is proposed. The final governing equation is deduced with the transfer matrix technique and a spring layer model based on the modified Hellinger-Reissner variational principle. One of the main superiorities of the present model is that the scale of final governing equation, which involves only the so-called state variables at the top and bottom surfaces, is insensitive to the thickness and the number of layers of composite laminates. Several relevant numerical examples are carried out to validate the present model, and the present results are in good agreement with pre-existing results. |
topic |
composite laminate delamination local radial point interpolation method mechanical buckling thermal buckling |
url |
https://doi.org/10.1515/secm-2015-0003 |
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