Free Vibration Analysis of Fiber Metal Laminated Straight Beam
In recent years, studies on the development of new and advanced composite materials have been increasing. Among these new technological products, Fiber Metal Laminates (FML), and hybrid structures made of aluminium, carbon, glass or aramid fiber, are preferred especially in the aircraft industry due...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
De Gruyter
2018-10-01
|
| Series: | Open Chemistry |
| Subjects: | |
| Online Access: | http://www.degruyter.com/view/j/chem.2018.16.issue-1/chem-2018-0101/chem-2018-0101.xml?format=INT |
| _version_ | 1828369695804227584 |
|---|---|
| author | Maraş Sinan Yaman Mustafa Şansveren Mehmet Fatih Reyhan Sina Karimpour |
| author_facet | Maraş Sinan Yaman Mustafa Şansveren Mehmet Fatih Reyhan Sina Karimpour |
| author_sort | Maraş Sinan |
| collection | DOAJ |
| description | In recent years, studies on the development of new and advanced composite materials have been increasing. Among these new technological products, Fiber Metal Laminates (FML), and hybrid structures made of aluminium, carbon, glass or aramid fiber, are preferred especially in the aircraft industry due to their high performance. Therefore, free vibration analysis is necessary for the design process of such structures. In this study, the vibration characteristics of FML for clamped-free boundary conditions were investigated experimentally and numerically. Firstly, numerical results were obtained using Finite Element Method (FEM) and then these results were compared with the experimental results. It was seen that the numerical results were in good agreement with the experimental results. As the theoretical model was justified, the effects of various parameters such as number of layers, fiber orientations, and aluminium layer thickness on the in-plane vibration characteristics of the FML straight beam were analysed using FEM. Thus, most important parameters affecting the vibration characteristics of the hybrid structures were determined. |
| first_indexed | 2024-04-14T06:28:03Z |
| format | Article |
| id | doaj.art-824e90395a0848b39ac20a0748246a3d |
| institution | Directory Open Access Journal |
| issn | 2391-5420 |
| language | English |
| last_indexed | 2024-04-14T06:28:03Z |
| publishDate | 2018-10-01 |
| publisher | De Gruyter |
| record_format | Article |
| series | Open Chemistry |
| spelling | doaj.art-824e90395a0848b39ac20a0748246a3d2022-12-22T02:07:44ZengDe GruyterOpen Chemistry2391-54202018-10-0116194494810.1515/chem-2018-0101chem-2018-0101Free Vibration Analysis of Fiber Metal Laminated Straight BeamMaraş Sinan0Yaman Mustafa1Şansveren Mehmet Fatih2Reyhan Sina Karimpour3Bayburt University/Mechanical Engineering Department, Bayburt, TurkeyAtatürk University/Mechanical Engineering Department, Erzurum, TurkeyAtatürk University/Mechanical Engineering Department, Erzurum, TurkeyAtatürk University/Mechanical Engineering Department, Erzurum, TurkeyIn recent years, studies on the development of new and advanced composite materials have been increasing. Among these new technological products, Fiber Metal Laminates (FML), and hybrid structures made of aluminium, carbon, glass or aramid fiber, are preferred especially in the aircraft industry due to their high performance. Therefore, free vibration analysis is necessary for the design process of such structures. In this study, the vibration characteristics of FML for clamped-free boundary conditions were investigated experimentally and numerically. Firstly, numerical results were obtained using Finite Element Method (FEM) and then these results were compared with the experimental results. It was seen that the numerical results were in good agreement with the experimental results. As the theoretical model was justified, the effects of various parameters such as number of layers, fiber orientations, and aluminium layer thickness on the in-plane vibration characteristics of the FML straight beam were analysed using FEM. Thus, most important parameters affecting the vibration characteristics of the hybrid structures were determined.http://www.degruyter.com/view/j/chem.2018.16.issue-1/chem-2018-0101/chem-2018-0101.xml?format=INTFiber Metal LaminatesLaminated Composite Straight BeamVibration AnalysisFinite Element MethodHybrid Structures |
| spellingShingle | Maraş Sinan Yaman Mustafa Şansveren Mehmet Fatih Reyhan Sina Karimpour Free Vibration Analysis of Fiber Metal Laminated Straight Beam Open Chemistry Fiber Metal Laminates Laminated Composite Straight Beam Vibration Analysis Finite Element Method Hybrid Structures |
| title | Free Vibration Analysis of Fiber Metal Laminated Straight Beam |
| title_full | Free Vibration Analysis of Fiber Metal Laminated Straight Beam |
| title_fullStr | Free Vibration Analysis of Fiber Metal Laminated Straight Beam |
| title_full_unstemmed | Free Vibration Analysis of Fiber Metal Laminated Straight Beam |
| title_short | Free Vibration Analysis of Fiber Metal Laminated Straight Beam |
| title_sort | free vibration analysis of fiber metal laminated straight beam |
| topic | Fiber Metal Laminates Laminated Composite Straight Beam Vibration Analysis Finite Element Method Hybrid Structures |
| url | http://www.degruyter.com/view/j/chem.2018.16.issue-1/chem-2018-0101/chem-2018-0101.xml?format=INT |
| work_keys_str_mv | AT marassinan freevibrationanalysisoffibermetallaminatedstraightbeam AT yamanmustafa freevibrationanalysisoffibermetallaminatedstraightbeam AT sansverenmehmetfatih freevibrationanalysisoffibermetallaminatedstraightbeam AT reyhansinakarimpour freevibrationanalysisoffibermetallaminatedstraightbeam |