Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites
Polymeric composites have gone through a level of maturity beyond the laboratory stage with the development of the Boeing 787, the structure of which contains more than 50% composites. Nonetheless, a basic understanding of the material used in its primary structure has not been extensively investiga...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | en_US |
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John Wiley & Sons, Inc.
2012
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| Online Access: | http://hdl.handle.net/1721.1/70009 https://orcid.org/0000-0003-3530-5819 |
| _version_ | 1826188546731409408 |
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| author | Drakonakis, Vasileios M. Velisaris, Chris N. Seferis, James C. Doumanidis, Charalambos C. Wardle, Brian L. Papanicolaou, George C. |
| author2 | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics |
| author_facet | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Drakonakis, Vasileios M. Velisaris, Chris N. Seferis, James C. Doumanidis, Charalambos C. Wardle, Brian L. Papanicolaou, George C. |
| author_sort | Drakonakis, Vasileios M. |
| collection | MIT |
| description | Polymeric composites have gone through a level of maturity beyond the laboratory stage with the development of the Boeing 787, the structure of which contains more than 50% composites. Nonetheless, a basic understanding of the material used in its primary structure has not been extensively investigated. For instance, micromechanical models are inadequate as they always assume an evenly distributed homogeneous matrix, without following classic lamination theory, which assumes constant stress through the laminate thickness. Our program now in its third year at the Polymeric Composites Laboratory in Seattle, supported by industry as well as government agencies, and in collaboration with several universities on a global scale, is developing such concepts for understanding and improving matrices in layered configurations. This effort focuses on the development of interlayer systems used as enablers to improve certain properties of the composite, such as fracture-toughness and crack-propagation inhibition. POLYM. COMPOS., 31:1965–1976, 2010. |
| first_indexed | 2024-09-23T08:01:23Z |
| format | Article |
| id | mit-1721.1/70009 |
| institution | Massachusetts Institute of Technology |
| language | en_US |
| last_indexed | 2024-09-23T08:01:23Z |
| publishDate | 2012 |
| publisher | John Wiley & Sons, Inc. |
| record_format | dspace |
| spelling | mit-1721.1/700092022-09-30T01:44:16Z Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites Drakonakis, Vasileios M. Velisaris, Chris N. Seferis, James C. Doumanidis, Charalambos C. Wardle, Brian L. Papanicolaou, George C. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Drakonakis, Vasileios M. Wardle, Brian L. Drakonakis, Vasileios M. Polymeric composites have gone through a level of maturity beyond the laboratory stage with the development of the Boeing 787, the structure of which contains more than 50% composites. Nonetheless, a basic understanding of the material used in its primary structure has not been extensively investigated. For instance, micromechanical models are inadequate as they always assume an evenly distributed homogeneous matrix, without following classic lamination theory, which assumes constant stress through the laminate thickness. Our program now in its third year at the Polymeric Composites Laboratory in Seattle, supported by industry as well as government agencies, and in collaboration with several universities on a global scale, is developing such concepts for understanding and improving matrices in layered configurations. This effort focuses on the development of interlayer systems used as enablers to improve certain properties of the composite, such as fracture-toughness and crack-propagation inhibition. POLYM. COMPOS., 31:1965–1976, 2010. United States. Air Force Office of Scientific Research GloCal Network Corporation 2012-04-13T14:14:36Z 2012-04-13T14:14:36Z 2010-05 Article http://purl.org/eprint/type/JournalArticle 0272-8397 1548-0569 http://hdl.handle.net/1721.1/70009 Drakonakis, Vasileios M. et al. “Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites.” Polymer Composites 31.11 (2010): 1965–1976. Web. https://orcid.org/0000-0003-3530-5819 en_US http://dx.doi.org/10.1002/pc.20996 Polymer Composites Creative Commons Attribution-Noncommercial-Share Alike 3.0 http://creativecommons.org/licenses/by-nc-sa/3.0/ application/pdf John Wiley & Sons, Inc. Wardle (via assistant) |
| spellingShingle | Drakonakis, Vasileios M. Velisaris, Chris N. Seferis, James C. Doumanidis, Charalambos C. Wardle, Brian L. Papanicolaou, George C. Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites |
| title | Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites |
| title_full | Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites |
| title_fullStr | Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites |
| title_full_unstemmed | Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites |
| title_short | Matrix Hybridization in the Interlayer for Carbon Fiber Reinforced Composites |
| title_sort | matrix hybridization in the interlayer for carbon fiber reinforced composites |
| url | http://hdl.handle.net/1721.1/70009 https://orcid.org/0000-0003-3530-5819 |
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