TY  - JOUR
AU  - Bisagni, C.
AU  - Raimondo, A.
AU  - Atanasovska, Ivana
AU  - Milić, M.
AU  - Troian, R.
AU  - Frulla, G.
AU  - Polla, A.
AU  - Cora, Ö.N.
AU  - Bekci, M.L.
AU  - Henriques, B.
AU  - de Moura, M.F.S.F.
AU  - Almudaihesh, F.
AU  - Grigg, S.
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3824
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.
PB  - Elsevier B.V.
T2  - Composites Part C: Open Access
T1  - Comparison of numerical analyses of a composite wing component subjected to 4-point bending
VL  - 8
DO  - 10.1016/j.jcomc.2022.100264
ER  - 

@article{
author = "Bisagni, C. and Raimondo, A. and Atanasovska, Ivana and Milić, M. and Troian, R. and Frulla, G. and Polla, A. and Cora, Ö.N. and Bekci, M.L. and Henriques, B. and de Moura, M.F.S.F. and Almudaihesh, F. and Grigg, S.",
year = "2022",
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.",
publisher = "Elsevier B.V.",
journal = "Composites Part C: Open Access",
title = "Comparison of numerical analyses of a composite wing component subjected to 4-point bending",
volume = "8",
doi = "10.1016/j.jcomc.2022.100264"
}

Bisagni, C., Raimondo, A., Atanasovska, I., Milić, M., Troian, R., Frulla, G., Polla, A., Cora, Ö.N., Bekci, M.L., Henriques, B., de Moura, M.F.S.F., Almudaihesh, F.,& Grigg, S.. (2022). Comparison of numerical analyses of a composite wing component subjected to 4-point bending. in Composites Part C: Open Access
Elsevier B.V.., 8.
https://doi.org/10.1016/j.jcomc.2022.100264

Bisagni C, Raimondo A, Atanasovska I, Milić M, Troian R, Frulla G, Polla A, Cora Ö, Bekci M, Henriques B, de Moura M, Almudaihesh F, Grigg S. Comparison of numerical analyses of a composite wing component subjected to 4-point bending. in Composites Part C: Open Access. 2022;8.
doi:10.1016/j.jcomc.2022.100264 .

Bisagni, C., Raimondo, A., Atanasovska, Ivana, Milić, M., Troian, R., Frulla, G., Polla, A., Cora, Ö.N., Bekci, M.L., Henriques, B., de Moura, M.F.S.F., Almudaihesh, F., Grigg, S., "Comparison of numerical analyses of a composite wing component subjected to 4-point bending" in Composites Part C: Open Access, 8 (2022),
https://doi.org/10.1016/j.jcomc.2022.100264 . .