Zobrazeno 1 - 10
of 37
pro vyhledávání: '"Vincenzo Oliveri"'
Publikováno v:
Materials & Design, Vol 206, Iss , Pp 109769- (2021)
Composite materials can enhance morphing and deployable structure capability due to their high degree of tailorability and their favourable stiffness- and strength-to-weight ratios. One such structure, the bistable helical lattice, is augmented in cu
Externí odkaz:
https://doaj.org/article/ae482a76a2ab4e72bdfc6828f19a37ee
Publikováno v:
AIAA Journal. :1-18
Since the introduction of variable-stiffness composites, the design philosophy for high-performance lightweight composite structures has broadened greatly. Indeed, variable-stiffness composites have been shown to increase buckling performance and dyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a082145b964564101e7b7c1ee3618387
https://doi.org/10.2514/1.j062890
https://doi.org/10.2514/1.j062890
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2514c809f95a38d60f275c758144452
https://doi.org/10.2514/6.2023-1322.c1
https://doi.org/10.2514/6.2023-1322.c1
Autor:
Mohammad Rouhi, Paul M. Weaver, Ronan M. O'Higgins, Enzo Cosentino, Giovanni Zucco, Vincenzo Oliveri
Publikováno v:
AIAA Journal. 59:5117-5129
Cutouts are widely used to accommodate windows, openings for access purposes, or fasteners in the primary structural parts of airplanes. The presence of cutouts in composite panels results in stres...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eaaeaa7f3cfbd0851360748a32dd6b32
https://doi.org/10.2514/1.j060668
https://doi.org/10.2514/1.j060668
A Ritz formulation for non-linear analysis of damage initiation and evolution in variable angle tow composite plates under progressive loading is presented. The model is built on a few key items. It assumes first order shear deformation theory kinema
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bbc7d17cfc68eb054692c419ac583876
https://hdl.handle.net/10447/583338
https://hdl.handle.net/10447/583338
Autor:
Enzo Cosentino, Ronan M. O'Higgins, Vincenzo Oliveri, Giovanni Zucco, Paul M. Weaver, Trevor M. Young, Mohammad Rouhi
Publikováno v:
American Society for Composites 2021.
The design of a multi-part aerospace structural component, such as a wingbox, is a challenging process because of the complexity arising from assembly and integration, and their associated limitations and considerations. In this study, a design proce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca03d691b9b02f28e05c72888171829b
https://doi.org/10.12783/asc36/35766
https://doi.org/10.12783/asc36/35766
Publikováno v:
Scopus-Elsevier
With the introduction of the variable stiffness concept, the design space for highperformance lightweight composite structures has expanded significantly. A larger design space, in particular, allows designers to find more effective solutions with hi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::762ed193c2d6ad53921579c51af5d757
https://doi.org/10.12783/asc36/35926
https://doi.org/10.12783/asc36/35926
Autor:
Alberto Milazzo, Vincenzo Oliveri
Variable Angle Tow (VAT) composite plates are characterized by in-plane variable stiffness properties, which opens to new concepts of stiffness tailoring and optimization to achieve higher structural performance for advanced lightweight structures wh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c6562d3a82ddfd12b6bfeb7bd9345dcf
http://hdl.handle.net/10447/515275
http://hdl.handle.net/10447/515275
Autor:
Gearóid J. Clancy, Ciarán McHale, Vincenzo Oliveri, Trevor M. Young, Daniël Peeters, Robert Telford, Paul M. Weaver, Giovanni Zucco, Ronan M. O'Higgins, Mohammad Rouhi
Publikováno v:
AIAA Journal. 57:1671-1683
Thermoplastic composites offer the potential for reducing the overall manufacturing costs of aircraft structures by allowing continuous production methods to be applied without the ancillary need f...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33460dd43381009e9abbd6a4692b9554
https://doi.org/10.2514/1.j057758
https://doi.org/10.2514/1.j057758
Autor:
Paul M. Weaver, Vincenzo Oliveri, Gearóid J. Clancy, Ronan M. O'Higgins, Daniël Peeters, David Jones
Publikováno v:
Composite Structures. 212:271-280
Fibre reinforced composite materials are finding increasing application in aerospace structures due to their superior specific properties. Aerospace structures make widespread use of stiffening elements, such as stringers, for example in wingboxes an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8bde79cc3ee667561f512f1c7d3aee8d
https://doi.org/10.1016/j.compstruct.2019.01.033
https://doi.org/10.1016/j.compstruct.2019.01.033