Failure Analysis of CFRP Multidirectional Laminates Using the Probabilistic Weibull Distribution Model under Static Loading
The application of carbon fiber reinforced polymer (CFRP) Multidirectional (MD) laminates in aircraft structure have motivated the manufacturers to tailor the mechanical strength in desired directions. The complex stress field owing to multiple orientations with the loading direction increases the i...
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| Published in | Fibers and polymers Vol. 20; no. 11; pp. 2390 - 2399 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Seoul
The Korean Fiber Society
01.11.2019
Springer Nature B.V 한국섬유공학회 |
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| Online Access | Get full text |
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| Abstract | The application of carbon fiber reinforced polymer (CFRP) Multidirectional (MD) laminates in aircraft structure have motivated the manufacturers to tailor the mechanical strength in desired directions. The complex stress field owing to multiple orientations with the loading direction increases the intricacy of failure analysis. Hence, the macroscopic and microscopic fracture behaviour of MD CFRP laminates under static loading needs to be explored further. In this study, four different MD CFRP laminates were fabricated using IMA/M21 prepregs by the autoclaving technique. Effect of fiber orientation on static strength i.e. tensile and compressive strength was studied. The strength decreased with the increase in orientation angle. Scanning electron micrographs revealed that irrespective of the lay-up sequence individual layers failed parallel to the fiber direction. Fiber breakage and delamination were the major failure modes in tensile specimens while kinking, matrix failure, in-plane shear, stepped fracture, and fiber-matrix debonding were dominated in compression specimens. The theoretical and experimental data was in good agreement with the Weibull distribution model. |
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| AbstractList | The application of carbon fiber reinforced polymer (CFRP) Multidirectional (MD) laminates in aircraft structure have motivated the manufacturers to tailor the mechanical strength in desired directions. The complex stress field owing to multiple orientations with the loading direction increases the intricacy of failure analysis. Hence, the macroscopic and microscopic fracture behaviour of MD CFRP laminates under static loading needs to be explored further. In this study, four different MD CFRP laminates were fabricated using IMA/M21 prepregs by the autoclaving technique. Effect of fiber orientation on static strength i.e. tensile and compressive strength was studied. The strength decreased with the increase in orientation angle. Scanning electron micrographs revealed that irrespective of the lay-up sequence individual layers failed parallel to the fiber direction. Fiber breakage and delamination were the major failure modes in tensile specimens while kinking, matrix failure, in-plane shear, stepped fracture, and fiber-matrix debonding were dominated in compression specimens. The theoretical and experimental data was in good agreement with the Weibull distribution model. The application of carbon fiber reinforced polymer (CFRP) Multidirectional (MD) laminates in aircraft structurehave motivated the manufacturers to tailor the mechanical strength in desired directions. The complex stress field owing tomultiple orientations with the loading direction increases the intricacy of failure analysis. Hence, the macroscopic andmicroscopic fracture behaviour of MD CFRP laminates under static loading needs to be explored further. In this study, fourdifferent MD CFRP laminates were fabricated using IMA/M21 prepregs by the autoclaving technique. Effect of fiberorientation on static strength i.e. tensile and compressive strength was studied. The strength decreased with the increase inorientation angle. Scanning electron micrographs revealed that irrespective of the lay-up sequence individual layers failedparallel to the fiber direction. Fiber breakage and delamination were the major failure modes in tensile specimens whilekinking, matrix failure, in-plane shear, stepped fracture, and fiber-matrix debonding were dominated in compressionspecimens. The theoretical and experimental data was in good agreement with the Weibull distribution model. KCI Citation Count: 1 |
| Author | Behera, Alok Thawre, Manjusha M. Ballal, Atul |
| Author_xml | – sequence: 1 givenname: Alok surname: Behera fullname: Behera, Alok email: alokab132@gmail.com organization: Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT) – sequence: 2 givenname: Manjusha M. surname: Thawre fullname: Thawre, Manjusha M. organization: Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT) – sequence: 3 givenname: Atul surname: Ballal fullname: Ballal, Atul organization: Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT) |
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| Keywords | Multidirectional Compressive strength SEM CFRP Tensile strength |
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| Snippet | The application of carbon fiber reinforced polymer (CFRP) Multidirectional (MD) laminates in aircraft structure have motivated the manufacturers to tailor the... The application of carbon fiber reinforced polymer (CFRP) Multidirectional (MD) laminates in aircraft structurehave motivated the manufacturers to tailor the... |
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| SubjectTerms | Aircraft structures Autoclaving Breakage Carbon fiber reinforced plastics Chemistry Chemistry and Materials Science Compressive strength Delamination Electron micrographs Failure analysis Failure modes Fiber orientation Fiber reinforced polymers Kinking Laminates Orientation effects Polymer Sciences Prepregs Statistical analysis Stress concentration Stress distribution Tensile strength Weibull distribution 섬유공학 |
| Title | Failure Analysis of CFRP Multidirectional Laminates Using the Probabilistic Weibull Distribution Model under Static Loading |
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