Optimization of Fiber-Reinforced Laminates for a Maximum Fatigue Life by Using the Particle Swarm Optimization. Part II
An improved methodology, with considering experimental results and numerical models, is proposed to find globally optimum designs of composite laminates subject to given in-plane loads for a maximum fatigue life. For this purpose, the Fawaz–Ellyin parametric fatigue-life prediction model was coupled...
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| Veröffentlicht in: | Mechanics of composite materials Jg. 49; H. 1; S. 107 - 116 |
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| Format: | Journal Article |
| Sprache: | Englisch |
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01.03.2013
Springer |
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| ISSN: | 0191-5665, 1573-8922 |
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| Abstract | An improved methodology, with considering experimental results and numerical models, is proposed to find globally optimum designs of composite laminates subject to given in-plane loads for a maximum fatigue life. For this purpose, the Fawaz–Ellyin parametric fatigue-life prediction model was coupled with a global optimization technique, the particle swarm optimization, which is a metaheuristic optimization algorithm. The number of distinct fiber orientation angles and the number of plies in each lamina were predetermined. The fiber orientation angles in each layer were taken as design variables and determined in the design process. A number of problems were solved to demonstrate the efficiency and reliability of the method proposed. |
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| AbstractList | An improved methodology, with considering experimental results and numerical models, is proposed to find globally optimum designs of composite laminates subject to given in-plane loads for a maximum fatigue life. For this purpose, the Fawaz–Ellyin parametric fatigue-life prediction model was coupled with a global optimization technique, the particle swarm optimization, which is a metaheuristic optimization algorithm. The number of distinct fiber orientation angles and the number of plies in each lamina were predetermined. The fiber orientation angles in each layer were taken as design variables and determined in the design process. A number of problems were solved to demonstrate the efficiency and reliability of the method proposed. An improved methodology, with considering experimental results and numerical models, is proposed to find globally optimum designs of composite laminates subject to given in-plane loads for a maximum fatigue life. For this purpose, the Fawaz-Ellyin parametric fatigue-life prediction model was coupled with a global optimization technique, the particle swarm optimization, which is a metaheuristic optimization algorithm. The number of distinctfiber orientation angles and the number of plies in each lamina were predetermined. The fiber orientation angles in each layer were taken as design variables and determined in the design process. A number of problems were solved to demonstrate the efficiency and reliability of the method proposed. An improved methodology, with considering experimental results and numerical models, is proposed to find globally optimum designs of composite laminates subject to given in-plane loads for a maximum fatigue life. For this purpose, the FawazaEllyin parametric fatigue-life prediction model was coupled with a global optimization technique, the particle swarm optimization, which is a metaheuristic optimization algorithm. The number of distinct fiber orientation angles and the number of plies in each lamina were predetermined. The fiber orientation angles in each layer were taken as design variables and determined in the design process. A number of problems were solved to demonstrate the efficiency and reliability of the method proposed. An improved methodology, with considering experimental results and numerical models, is proposed to find globally optimum designs of composite laminates subject to given in-plane loads for a maximum fatigue life. For this purpose, the Fawaz-Ellyin parametric fatigue-life prediction model was coupled with a global optimization technique, the particle swarm optimization, which is a metaheuristic optimization algorithm. The number of distinctfiber orientation angles and the number of plies in each lamina were predetermined. The fiber orientation angles in each layer were taken as design variables and determined in the design process. A number of problems were solved to demonstrate the efficiency and reliability of the method proposed. Keywords: composites, fatigue life, Fawaz-Ellyin model, particle swarm optimization |
| Audience | Academic |
| Author | Ertas, Ahmet H. |
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| Cites_doi | 10.1016/j.eswa.2010.08.038 10.1016/0266-3538(94)00077-8 10.1016/j.compstruct.2006.09.007 10.1016/j.compstruct.2004.09.008 10.1016/j.proeng.2010.03.027 10.1080/03052150500384759 10.1177/002199839402801503 10.1007/s11029-013-9314-x 10.1016/j.compstruct.2006.10.008 10.1177/002199837300700404 10.1016/S0263-8223(99)00097-5 10.1109/ICNN.1995.488968 10.1201/9781420027839 |
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| Keywords | composites particle swarm optimization fatigue life Fawaz–Ellyin model |
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| References | Kathiravan, Ganguli (CR1) 2007; 81 Walker (CR6) 2000; 48 Eusuff, Lansey, Pasha (CR9) 2006; 38 Fawaz, Ellyin (CR11) 1994; 28 Ertas, Sonmez (CR7) 2010; 2 Ertas (CR17) 2012; 48 Adali, Marshall (CR5) 1986 CR8 CR16 CR14 CR13 CR12 Fawaz, Ellyin (CR10) 1995; 53 Hashin, Rotem (CR15) 1973; 7 Suresh, Sujit, Rao (CR2) 2007; 81 Erdal, Sonmez (CR4) 2005; 71 Narayana, Omkar, Mudigere, Gopalakrishnan (CR3) 2011; 38 R Kathiravan (9326_CR1) 2007; 81 9326_CR12 AH Ertas (9326_CR7) 2010; 2 9326_CR13 9326_CR14 9326_CR16 M Eusuff (9326_CR9) 2006; 38 Z Fawaz (9326_CR10) 1995; 53 Z Fawaz (9326_CR11) 1994; 28 S Adali (9326_CR5) 1986 M Walker (9326_CR6) 2000; 48 9326_CR8 Z Hashin (9326_CR15) 1973; 7 NG Narayana (9326_CR3) 2011; 38 S Suresh (9326_CR2) 2007; 81 O Erdal (9326_CR4) 2005; 71 AH Ertas (9326_CR17) 2012; 48 |
| References_xml | – volume: 38 start-page: 2489 year: 2011 end-page: 2499 ident: CR3 article-title: Nature-inspired optimization techniques for the design optimization of laminated composite structures using failure criteria publication-title: Expert Syst. Appl. doi: 10.1016/j.eswa.2010.08.038 – volume: 53 start-page: 47 issue: 1 year: 1995 end-page: 55 ident: CR10 article-title: A new methodology for the prediction of fatigue failure in multidirectional fiber-reinforced laminates publication-title: Compos. Sci. Technol. doi: 10.1016/0266-3538(94)00077-8 – volume: 81 start-page: 471 year: 2007 end-page: 479 ident: CR1 article-title: Strength design of composite beam using gradient and particle swarm optimization publication-title: Compos. Struct. doi: 10.1016/j.compstruct.2006.09.007 – volume: 71 start-page: 45 issue: 1 year: 2005 end-page: 52 ident: CR4 article-title: Optimum design of composite laminates for maximum buckling load capacity using simulated annealing publication-title: Compos. Struct. doi: 10.1016/j.compstruct.2004.09.008 – volume: 2 start-page: 251 year: 2010 end-page: 256 ident: CR7 article-title: Design of fiber-reinforced laminates for maximum fatigue life publication-title: Procedia Eng. doi: 10.1016/j.proeng.2010.03.027 – ident: CR14 – volume: 38 start-page: 129 issue: 2 year: 2006 end-page: 154 ident: CR9 article-title: Shuffled frog-leaping algorithm: a memetic meta-heuristic for discrete optimization publication-title: Eng. Optimiz. doi: 10.1080/03052150500384759 – ident: CR16 – ident: CR12 – ident: CR13 – volume: 28 start-page: 1432 issue: 15 year: 1994 end-page: 1451 ident: CR11 article-title: Fatigue failure model for fiber-reinforced materials under general loading conditions publication-title: J. Compos. Mater. doi: 10.1177/002199839402801503 – volume: 48 start-page: 705 issue: 6 year: 2012 end-page: 716 ident: CR17 article-title: Optimization of fiber- reinforced laminates for a maximum fatigue life by using the particle swarm optimization. Part I publication-title: Mech. Compos. Mater. doi: 10.1007/s11029-013-9314-x – volume: 81 start-page: 598 year: 2007 end-page: 605 ident: CR2 article-title: Particle swarm optimization approach for multiobjective composite box-beam design publication-title: Compos. Struct. doi: 10.1016/j.compstruct.2006.10.008 – volume: 7 start-page: 448 year: 1973 end-page: 464 ident: CR15 article-title: Fatigue failure criterion for fiber-reinforced materials publication-title: J. Compos. Mater. doi: 10.1177/002199837300700404 – ident: CR8 – volume: 48 start-page: 213 issue: 1–3 year: 2000 end-page: 218 ident: CR6 article-title: A method for optimally designing laminated plates subject to fatigue loads for minimum weight using a cumulative damage constraint publication-title: Compos. Struct. doi: 10.1016/S0263-8223(99)00097-5 – start-page: 43 year: 1986 end-page: 55 ident: CR5 article-title: Optimization of fibre reinforced composite Laminates Subject to Fatigue Loading publication-title: Composite Structures 3 – volume: 7 start-page: 448 year: 1973 ident: 9326_CR15 publication-title: J. Compos. Mater. doi: 10.1177/002199837300700404 – volume: 81 start-page: 471 year: 2007 ident: 9326_CR1 publication-title: Compos. Struct. doi: 10.1016/j.compstruct.2006.09.007 – volume: 71 start-page: 45 issue: 1 year: 2005 ident: 9326_CR4 publication-title: Compos. Struct. doi: 10.1016/j.compstruct.2004.09.008 – volume: 48 start-page: 705 issue: 6 year: 2012 ident: 9326_CR17 publication-title: Mech. Compos. Mater. doi: 10.1007/s11029-013-9314-x – volume: 38 start-page: 2489 year: 2011 ident: 9326_CR3 publication-title: Expert Syst. Appl. doi: 10.1016/j.eswa.2010.08.038 – volume: 2 start-page: 251 year: 2010 ident: 9326_CR7 publication-title: Procedia Eng. doi: 10.1016/j.proeng.2010.03.027 – ident: 9326_CR12 doi: 10.1109/ICNN.1995.488968 – ident: 9326_CR13 – ident: 9326_CR14 – volume: 48 start-page: 213 issue: 1–3 year: 2000 ident: 9326_CR6 publication-title: Compos. Struct. doi: 10.1016/S0263-8223(99)00097-5 – ident: 9326_CR8 – volume: 53 start-page: 47 issue: 1 year: 1995 ident: 9326_CR10 publication-title: Compos. Sci. Technol. doi: 10.1016/0266-3538(94)00077-8 – volume: 38 start-page: 129 issue: 2 year: 2006 ident: 9326_CR9 publication-title: Eng. Optimiz. doi: 10.1080/03052150500384759 – volume: 28 start-page: 1432 issue: 15 year: 1994 ident: 9326_CR11 publication-title: J. Compos. Mater. doi: 10.1177/002199839402801503 – start-page: 43 volume-title: Composite Structures 3 year: 1986 ident: 9326_CR5 – ident: 9326_CR16 doi: 10.1201/9781420027839 – volume: 81 start-page: 598 year: 2007 ident: 9326_CR2 publication-title: Compos. Struct. doi: 10.1016/j.compstruct.2006.10.008 |
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| SubjectTerms | Algorithms Analysis Ceramics Characterization and Evaluation of Materials Chemistry and Materials Science Classical Mechanics Composites Fatigue Fatigue life Fatigue testing machines Fiber orientation Glass Laminated materials Laminates Materials Materials Science Mathematical analysis Mathematical models Mathematical optimization Natural Materials Optimization Particulate composites Solid Mechanics |
| Title | Optimization of Fiber-Reinforced Laminates for a Maximum Fatigue Life by Using the Particle Swarm Optimization. Part II |
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