Fully Parametric Optimization Designs of Wing Components
An optimization technique called shape-linked optimization, which is different from the traditional optimization method, is introduced in this paper. The research introduces an updated wing optimization design in an effort to adapt to continuous structure changes and shapes while optimizing for a li...
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| Format: | Article |
| Language: | English |
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Wiley
2020-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2020/8841623 |
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| _version_ | 1849305136018489344 |
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| author | Zhendong Hu Ju Qiu Fa Zhang |
| author_facet | Zhendong Hu Ju Qiu Fa Zhang |
| author_sort | Zhendong Hu |
| collection | DOAJ |
| description | An optimization technique called shape-linked optimization, which is different from the traditional optimization method, is introduced in this paper. The research introduces an updated wing optimization design in an effort to adapt to continuous structure changes and shapes while optimizing for a lighter weight of the structure. The changing tendencies of the thickness of wing skins and the cross-section areas of the wing beams are fitted to continuous polynomial functions, whose coefficients are designed as variables, which is a different engineering approach from the size variants of the thickness and the area in the traditional optimization. The structural strength, stiffness, and stability are constraints. Firstly, this research unearths the significance of utilizing a modernized optimization process which alters the production of the traditional 12 or over 12 segment wing design and applies new approaches and methods with less variables that contribute to expedited design cycles, decreased engineering and manufacturing expenditures, and a lighter weight aircraft with lower operating costs than the traditional design for the operators. And then, this paper exemplifies and illustrates the validity of the above claims in a detailed and systematic approach by comparing traditional and modernized optimization applications with a two-beam wing. Finally, this paper also proves that the new optimized structure parameters are easier than the size optimization to process and manufacture. |
| format | Article |
| id | doaj-art-086dcfd91aa74f7abf040a1ff9036bc2 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2020-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-086dcfd91aa74f7abf040a1ff9036bc22025-08-20T03:55:32ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742020-01-01202010.1155/2020/88416238841623Fully Parametric Optimization Designs of Wing ComponentsZhendong Hu0Ju Qiu1Fa Zhang2Beijing Key Laboratory of Civil Aircraft Structures and Composite Materials, Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, ChinaBeijing Key Laboratory of Civil Aircraft Structures and Composite Materials, Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, ChinaBeijing Key Laboratory of Civil Aircraft Structures and Composite Materials, Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, ChinaAn optimization technique called shape-linked optimization, which is different from the traditional optimization method, is introduced in this paper. The research introduces an updated wing optimization design in an effort to adapt to continuous structure changes and shapes while optimizing for a lighter weight of the structure. The changing tendencies of the thickness of wing skins and the cross-section areas of the wing beams are fitted to continuous polynomial functions, whose coefficients are designed as variables, which is a different engineering approach from the size variants of the thickness and the area in the traditional optimization. The structural strength, stiffness, and stability are constraints. Firstly, this research unearths the significance of utilizing a modernized optimization process which alters the production of the traditional 12 or over 12 segment wing design and applies new approaches and methods with less variables that contribute to expedited design cycles, decreased engineering and manufacturing expenditures, and a lighter weight aircraft with lower operating costs than the traditional design for the operators. And then, this paper exemplifies and illustrates the validity of the above claims in a detailed and systematic approach by comparing traditional and modernized optimization applications with a two-beam wing. Finally, this paper also proves that the new optimized structure parameters are easier than the size optimization to process and manufacture.http://dx.doi.org/10.1155/2020/8841623 |
| spellingShingle | Zhendong Hu Ju Qiu Fa Zhang Fully Parametric Optimization Designs of Wing Components International Journal of Aerospace Engineering |
| title | Fully Parametric Optimization Designs of Wing Components |
| title_full | Fully Parametric Optimization Designs of Wing Components |
| title_fullStr | Fully Parametric Optimization Designs of Wing Components |
| title_full_unstemmed | Fully Parametric Optimization Designs of Wing Components |
| title_short | Fully Parametric Optimization Designs of Wing Components |
| title_sort | fully parametric optimization designs of wing components |
| url | http://dx.doi.org/10.1155/2020/8841623 |
| work_keys_str_mv | AT zhendonghu fullyparametricoptimizationdesignsofwingcomponents AT juqiu fullyparametricoptimizationdesignsofwingcomponents AT fazhang fullyparametricoptimizationdesignsofwingcomponents |