Stacking sequence optimisation of an aircraft wing skin

Autor: Georgios Ntourmas, Florian Glock, Sebastian Deinert, Fernass Daoud, Gerd Schuhmacher, Dimitrios Chronopoulos, Ender Özcan, Jelena Ninić

This paper demonstrates a stacking sequence optimisation process of a composite aircraft wing skin. A two-stage approach is employed to satisfy all sizing requirements of this industrial sized, medium altitude, long endurance drone. In the first stag

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::70909ab3eca10bc8b37e0825b64fde3c
https://lirias.kuleuven.be/handle/20.500.12942/716933

Mixed Integer Linear Programming formulations of the stacking sequence and blending optimisation of composite structures

Autor: Florian Glock, G. Ntourmas, Gerd Schuhmacher, Dimitrios Chronopoulos, F. Daoud, Ender Özcan

This manuscript proposes two novel formulations for the manufacturable stacking sequence retrieval of laminated composite structures . Detailed sizing of composite structures is commonly tackled by a two-stage optimisation approach, the first stage b

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f751aff02547c782c20a34cb4402094f
https://lirias.kuleuven.be/handle/123456789/681832

Lay-up Optimization of Laminated Composites Using a Modified Branch and Bound Method

Autor: Felice Rubino, Angelo Maligno, Giacomo Canale, Roberto Guglielmo Citarella, Paul M. Weaver

Background:Composite materials are widely used in the aerospace, marine and automotive industries. One of their main advantages is that their stacking sequence can be tailored to maximise/minimise a specific structural performance. Efficient and non-

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3fb9bb09148abedca3ee8c493755df68
http://hdl.handle.net/11386/4716946

Determination of the longitudinal compressive strength of a CFRP ply through a tensile test on a laminate

Autor: F. Laurin, François-Xavier Irisarri, Pascal Paulmier

Publikováno v: Composites Part A: Applied Science and Manufacturing
Composites Part A: Applied Science and Manufacturing, Elsevier, 2018, 113, pp.209-219. ⟨10.1016/j.compositesa.2018.07.026⟩

In this study, an innovative test is proposed to identify the longitudinal compressive strength of a unidirectional ply. The key idea consists in designing a laminate that, when subjected to a tensile loading, fails by compressive failure in its cent

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cb926eb4c8a116a46f5f7b9f214eff63
https://hal.archives-ouvertes.fr/hal-01870106

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