Sequential Quadratic Programming Method of Cabin Optimization
The basic principle of sequential quadratic programming method and the concrete implementation steps in MATLAB are expounded. Sequential quadratic programming method is used for the cabin structure optimization. In the optimization, the minimal sizes of components stipulated by the rules are used as...
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| Veröffentlicht in: | Applied Mechanics and Materials Jg. 711; H. Mechanical Engineering, Materials Science and Civil Engineering; S. 96 - 99 |
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| Hauptverfasser: | , , , |
| Format: | Journal Article |
| Sprache: | Englisch |
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Trans Tech Publications Ltd
01.12.2014
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| ISBN: | 9783038353720, 3038353728 |
| ISSN: | 1660-9336, 1662-7482, 1662-7482 |
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| Abstract | The basic principle of sequential quadratic programming method and the concrete implementation steps in MATLAB are expounded. Sequential quadratic programming method is used for the cabin structure optimization. In the optimization, the minimal sizes of components stipulated by the rules are used as size constraints, the frequencies required by the rules are used as performance constraints and the minimum lightness of the ship are used as objective. Finite element analysis of the ship structure optimized is done and the results obtained show that both the maximum equivalent stress and the maximum shear stress meet the requirements and first three order frequencies of the cabin structure are also far away from the working frequency of propeller and host. The optimization reduces the weight of the cabin under the condition of meet the static characteristic and dynamic characteristic. |
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| AbstractList | The basic principle of sequential quadratic programming method and the concrete implementation steps in MATLAB are expounded. Sequential quadratic programming method is used for the cabin structure optimization. In the optimization, the minimal sizes of components stipulated by the rules are used as size constraints, the frequencies required by the rules are used as performance constraints and the minimum lightness of the ship are used as objective. Finite element analysis of the ship structure optimized is done and the results obtained show that both the maximum equivalent stress and the maximum shear stress meet the requirements and first three order frequencies of the cabin structure are also far away from the working frequency of propeller and host. The optimization reduces the weight of the cabin under the condition of meet the static characteristic and dynamic characteristic. |
| Author | Liu, Han Song, Bo Song, Fang Zhen Li, Ming Ming |
| Author_xml | – givenname: Ming Ming surname: Li fullname: Li, Ming Ming organization: University of Jinan : School of Mechanical Engineering – givenname: Fang Zhen surname: Song fullname: Song, Fang Zhen email: me_songfz@ujn.edu.cn organization: University of Jinan : School of Mechanical Engineering – givenname: Han surname: Liu fullname: Liu, Han organization: University of Jinan : School of Mechanical Engineering – givenname: Bo surname: Song fullname: Song, Bo organization: University of Jinan : School of Mechanical Engineering |
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| Cites_doi | 10.1137/s0363012994261707 |
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| Copyright | 2015 Trans Tech Publications Ltd Copyright Trans Tech Publications Ltd. Dec 2014 |
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| Issue | Mechanical Engineering, Materials Science and Civil Engineering |
| Keywords | Frequency Sequential Quadratic Programming Method Optimization Stress |
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| StartPage | 96 |
| SubjectTerms | Cabins Equivalence Mathematical analysis Matlab Optimization Quadratic programming Shear stress Ships Weight reduction |
| Title | Sequential Quadratic Programming Method of Cabin Optimization |
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