Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase

Odeh Dababneh, Altan Kayran

Research output: Contribution to conferencePaper

Abstract

The article gives a comprehensive study on the effect of using different structural idealizations on the design, analysis and optimization of thin walled semi-monocoque wing structures in the preliminary design phase. In the design part of the article, wing structures are designed by employing two different structural idealizations that are typically used in the preliminary design phase. In the structural analysis part, finite element analysis of one of the designed wing configurations is performed using six different one and two dimensional element pairs which are typically used to model the sub-elements of semi-monocoque wing structures. The effect of using different finite element types on the analysis results of the wing structure, which is designed by the simplified method using two different idealization approaches, is investigated. Comparisons are also made between the analysis results of the finite element solution and the simplified method, and the applicability of the simplified method in the preliminary design phase is investigated for the wing configuration studied in the article. During the analysis study, depending on the mesh size used, conclusions are also inferred with regard to the deficiency of certain element types in handling the true external load acting on the wing structure. Finally in the optimization part, wing structure is optimized for minimum weight by using finite element models which have the same six different element pairs used in the analysis phase. The effect of using different one and two dimensional element pairs on the final optimized configurations of the wing structure is investigated, and conclusions are inferred with regard to the sensitivity of the optimized wing configurations with respect to the choice of different element types in the finite element model. Final optimized wing structure configurations are also compared with the simplified method based designs which are also optimized iteratively.
Original languageEnglish
Pages186-201
Publication statusPublished - Oct 2013
Event3rd EASN Association International Workshop on AeroStructures - Politico di milano, Milanao , Italy
Duration: 09 Oct 201311 Oct 2013
Conference number: 3

Conference

Conference3rd EASN Association International Workshop on AeroStructures
CountryItaly
CityMilanao
Period09/10/201311/10/2013

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Structural analysis
Finite element method

Cite this

Dababneh, O., & Kayran , A. (2013). Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. 186-201. Paper presented at 3rd EASN Association International Workshop on AeroStructures, Milanao , Italy.
Dababneh, Odeh ; Kayran , Altan . / Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. Paper presented at 3rd EASN Association International Workshop on AeroStructures, Milanao , Italy.
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abstract = "The article gives a comprehensive study on the effect of using different structural idealizations on the design, analysis and optimization of thin walled semi-monocoque wing structures in the preliminary design phase. In the design part of the article, wing structures are designed by employing two different structural idealizations that are typically used in the preliminary design phase. In the structural analysis part, finite element analysis of one of the designed wing configurations is performed using six different one and two dimensional element pairs which are typically used to model the sub-elements of semi-monocoque wing structures. The effect of using different finite element types on the analysis results of the wing structure, which is designed by the simplified method using two different idealization approaches, is investigated. Comparisons are also made between the analysis results of the finite element solution and the simplified method, and the applicability of the simplified method in the preliminary design phase is investigated for the wing configuration studied in the article. During the analysis study, depending on the mesh size used, conclusions are also inferred with regard to the deficiency of certain element types in handling the true external load acting on the wing structure. Finally in the optimization part, wing structure is optimized for minimum weight by using finite element models which have the same six different element pairs used in the analysis phase. The effect of using different one and two dimensional element pairs on the final optimized configurations of the wing structure is investigated, and conclusions are inferred with regard to the sensitivity of the optimized wing configurations with respect to the choice of different element types in the finite element model. Final optimized wing structure configurations are also compared with the simplified method based designs which are also optimized iteratively.",
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Dababneh, O & Kayran , A 2013, 'Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase', Paper presented at 3rd EASN Association International Workshop on AeroStructures, Milanao , Italy, 09/10/2013 - 11/10/2013 pp. 186-201.

Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. / Dababneh, Odeh; Kayran , Altan .

2013. 186-201 Paper presented at 3rd EASN Association International Workshop on AeroStructures, Milanao , Italy.

Research output: Contribution to conferencePaper

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N2 - The article gives a comprehensive study on the effect of using different structural idealizations on the design, analysis and optimization of thin walled semi-monocoque wing structures in the preliminary design phase. In the design part of the article, wing structures are designed by employing two different structural idealizations that are typically used in the preliminary design phase. In the structural analysis part, finite element analysis of one of the designed wing configurations is performed using six different one and two dimensional element pairs which are typically used to model the sub-elements of semi-monocoque wing structures. The effect of using different finite element types on the analysis results of the wing structure, which is designed by the simplified method using two different idealization approaches, is investigated. Comparisons are also made between the analysis results of the finite element solution and the simplified method, and the applicability of the simplified method in the preliminary design phase is investigated for the wing configuration studied in the article. During the analysis study, depending on the mesh size used, conclusions are also inferred with regard to the deficiency of certain element types in handling the true external load acting on the wing structure. Finally in the optimization part, wing structure is optimized for minimum weight by using finite element models which have the same six different element pairs used in the analysis phase. The effect of using different one and two dimensional element pairs on the final optimized configurations of the wing structure is investigated, and conclusions are inferred with regard to the sensitivity of the optimized wing configurations with respect to the choice of different element types in the finite element model. Final optimized wing structure configurations are also compared with the simplified method based designs which are also optimized iteratively.

AB - The article gives a comprehensive study on the effect of using different structural idealizations on the design, analysis and optimization of thin walled semi-monocoque wing structures in the preliminary design phase. In the design part of the article, wing structures are designed by employing two different structural idealizations that are typically used in the preliminary design phase. In the structural analysis part, finite element analysis of one of the designed wing configurations is performed using six different one and two dimensional element pairs which are typically used to model the sub-elements of semi-monocoque wing structures. The effect of using different finite element types on the analysis results of the wing structure, which is designed by the simplified method using two different idealization approaches, is investigated. Comparisons are also made between the analysis results of the finite element solution and the simplified method, and the applicability of the simplified method in the preliminary design phase is investigated for the wing configuration studied in the article. During the analysis study, depending on the mesh size used, conclusions are also inferred with regard to the deficiency of certain element types in handling the true external load acting on the wing structure. Finally in the optimization part, wing structure is optimized for minimum weight by using finite element models which have the same six different element pairs used in the analysis phase. The effect of using different one and two dimensional element pairs on the final optimized configurations of the wing structure is investigated, and conclusions are inferred with regard to the sensitivity of the optimized wing configurations with respect to the choice of different element types in the finite element model. Final optimized wing structure configurations are also compared with the simplified method based designs which are also optimized iteratively.

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Dababneh O, Kayran A. Design, Analysis and Optimization of Thin Walled Semi-Monocoque Wing Structures Using Different Structural Idealizations in the Preliminary Design Phase. 2013. Paper presented at 3rd EASN Association International Workshop on AeroStructures, Milanao , Italy.