Comparison of numerical analyses of a composite wing component subjected to 4-point bending

C. Bisagni; A. Raimondo; I. Atanasovska; M. Milic; R. Troian; G. Frulla; A. Polla; N. Cora; M. L. Bekci; null More Authors

doi:10.1016/j.jcomc.2022.100264

Comparison of numerical analyses of a composite wing component subjected to 4-point bending

C. Bisagni^*, A. Raimondo, I. Atanasovska, M. Milic, R. Troian, G. Frulla, A. Polla, N. Cora, M. L. Bekci, More Authors

^*Corresponding author for this work

Aerospace Structures & Computational Mechanics

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Abstract

In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University.

Original language	English
Article number	100264
Number of pages	13
Journal	Composites Part C: Open Access
Volume	8
DOIs	https://doi.org/10.1016/j.jcomc.2022.100264
Publication status	Published - 2022

Keywords

Aerospace composite structure
Numerical benchmark
Wing structure

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10.1016/j.jcomc.2022.100264

1-s2.0-S2666682022000317-mainFinal published version, 17.9 MBLicence: CC BY

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title = "Comparison of numerical analyses of a composite wing component subjected to 4-point bending",

abstract = "In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University.",

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T1 - Comparison of numerical analyses of a composite wing component subjected to 4-point bending

AU - Bisagni, C.

AU - Raimondo, A.

AU - Atanasovska, I.

AU - Milic, M.

AU - Troian, R.

AU - Frulla, G.

AU - Polla, A.

AU - Cora, N.

AU - Bekci, M. L.

AU - More Authors, null

PY - 2022

Y1 - 2022

N2 - In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University.

AB - In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University.

KW - Aerospace composite structure

KW - Numerical benchmark

KW - Wing structure

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DO - 10.1016/j.jcomc.2022.100264

M3 - Article

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SN - 2666-6820

VL - 8

JO - Composites Part C: Open Access

JF - Composites Part C: Open Access

M1 - 100264

ER -

Comparison of numerical analyses of a composite wing component subjected to 4-point bending

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