Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures
The eight-node solid-shell finite element models have been developed for the analysis of laminated composite pate/shell structures with piezoelectric actuators and sensors. To resolve the locking problems of the solid-shell elements in laminated materials and improve accuracy, the assumed natural st...
| Main Authors: | , |
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| Format: | Article |
| Language: | en_US |
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2003
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| Online Access: | http://hdl.handle.net/1721.1/3988 |
| _version_ | 1826208806460194816 |
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| author | Yi, Sung Yao, Lin-Quan |
| author_facet | Yi, Sung Yao, Lin-Quan |
| author_sort | Yi, Sung |
| collection | MIT |
| description | The eight-node solid-shell finite element models have been developed for the analysis of laminated composite pate/shell structures with piezoelectric actuators and sensors. To resolve the locking problems of the solid-shell elements in laminated materials and improve accuracy, the assumed natural strain method and hybrid stress method are employed. The nonlinear electric potential distribution in piezoelectric layer is described by introducing internal electric potential. The developed finite element models, especially, electric potential node model, have the advantages of simpler modeling and can obtain same effect that exact solution described. |
| first_indexed | 2024-09-23T14:12:37Z |
| format | Article |
| id | mit-1721.1/3988 |
| institution | Massachusetts Institute of Technology |
| language | en_US |
| last_indexed | 2024-09-23T14:12:37Z |
| publishDate | 2003 |
| record_format | dspace |
| spelling | mit-1721.1/39882019-04-10T08:59:52Z Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures Yi, Sung Yao, Lin-Quan laminate composite structure piezoelectric material finite element method hybrid stress element The eight-node solid-shell finite element models have been developed for the analysis of laminated composite pate/shell structures with piezoelectric actuators and sensors. To resolve the locking problems of the solid-shell elements in laminated materials and improve accuracy, the assumed natural strain method and hybrid stress method are employed. The nonlinear electric potential distribution in piezoelectric layer is described by introducing internal electric potential. The developed finite element models, especially, electric potential node model, have the advantages of simpler modeling and can obtain same effect that exact solution described. Singapore-MIT Alliance (SMA) 2003-12-22T20:52:36Z 2003-12-22T20:52:36Z 2002-01 Article http://hdl.handle.net/1721.1/3988 en_US Advanced Materials for Micro- and Nano-Systems (AMMNS); 136441 bytes application/pdf application/pdf |
| spellingShingle | laminate composite structure piezoelectric material finite element method hybrid stress element Yi, Sung Yao, Lin-Quan Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures |
| title | Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures |
| title_full | Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures |
| title_fullStr | Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures |
| title_full_unstemmed | Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures |
| title_short | Solid-shell element model of assumed through-thickness electric distribution for laminate composite piezoelectric structures |
| title_sort | solid shell element model of assumed through thickness electric distribution for laminate composite piezoelectric structures |
| topic | laminate composite structure piezoelectric material finite element method hybrid stress element |
| url | http://hdl.handle.net/1721.1/3988 |
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