Výsledky vyhledávání - "F, Scaramuzzino"

Numerical Investigation of the Failure Phenomena in Adhesively Bonded Joints by Means of a Multi-Linear Equivalent Plastic Stress/Strain Approach

Autor: Aniello Riccio, Debora Di Caprio, R. Ricchiuto, A. Raimondo, Andrea Sellitto, F. Scaramuzzino

Publikováno v: Procedia Engineering. 167:168-175

In this work, a multi-linear material model for elastic-plastic response of ductile adhesives is proposed. Indeed, the proposed formulation allows to evaluate equivalent stress and strains to be used as material model input in FE commercial codes ins

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b0843be16d16217c460c999719608b93

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Diagnostic role of detecting HPV in a FNAC of metastatic laterocervical lymph node in a case of occult HPV-related head and neck squamous cell carcinoma

Autor: A, Ginori, F, Scaramuzzino, M A G, Munezero Butorano, A, Barone, A, Disanto

Publikováno v: Pathologica. 108(2)

Human papillomavirus (HPV)-related head and neck squamous cell carcinomas (HNSCC) are radiosensitive tumors and have a better prognosis than the conventional keratinizing HNSCC. Despite extensive radiographic and clinical evaluation in approximately

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=pmid________::a39b191b22aee29fca198d4d4b4cdc69
https://pubmed.ncbi.nlm.nih.gov/28195253

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Modeling Delamination Growth in Composite Panels Subjected to Fatigue Load

Autor: Andrea Sellitto, F. Ronza, F. Scaramuzzino, Aniello Riccio

Publikováno v: Key Engineering Materials. 627:21-24

One of the most critical aspects of composite structures is indeed associated to delamination phenomenon, especially with reference to their fatigue behavior. As a matter of facts, delaminations are strongly influenced by the fatigue induced degradat

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c87336f5c5a1188f66e6a66e7c3f542c
https://doi.org/10.4028/www.scientific.net/kem.627.21

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Trade-off between paraffin-based and aluminium-loaded HTPB fuels to improve performance of hybrid rocket fed with N2O

Autor: Carmine Carmicino, A. Russo Sorge, F. Scaramuzzino

Publikováno v: Aerospace Science and Technology. 37:81-92

In the effort of raising the slow fuel-regression rate of hybrid rockets, two approaches focused on the fuel nature, i.e. the inclusion of metal particles into classical HTPB grains and the use of paraffin-wax based fuels, are investigated and contra

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::cb02779e48edb241c172c2cff88af83f
https://doi.org/10.1016/j.ast.2014.05.010

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Three-dimensional modeling of composites fire behavior

Autor: M. Damiano, Mauro Zarrelli, Aniello Riccio, F. Scaramuzzino

Publikováno v: Journal of reinforced plastics and composites
33 (2014): 619–629. doi:10.1177/0731684413512226
info:cnr-pdr/source/autori:Riccio, A.; Damiano, M.; Zarrelli, M.; Scaramuzzino, F./titolo:Three-dimensional modeling of composites fire behavior/doi:10.1177%2F0731684413512226/rivista:Journal of reinforced plastics and composites (Print)/anno:2014/pagina_da:619/pagina_a:629/intervallo_pagine:619–629/volume:33

The present paper introduces a numerical study on the fire behavior of composites during exposure to a heating source at high-incident power. A three-dimensional novel numerical model is proposed, which is able to simulate the behavior of composite m

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3bf86fc85f127e4b10eee0b226a195d1
https://doi.org/10.1177/0731684413512226

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Numerical Simulations of Inter-laminar Damage Evolution in a Composite Wing Box

Autor: Umberto Mercurio, F. Scaramuzzino, Domenico Tescione, Aniello Riccio, Rosario Borrelli, A. Raimondo

Publikováno v: Applied Composite Materials. 21:467-481

In this paper, a numerical study has been carried out on skin delamination and skin-stringer debonding growth in a composite wing-box under compressive loading conditions. The adopted numerical models use the Virtual Crack Closure Technique to simula

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1a6b0415350f20be7a25ab2abf16b35e
https://doi.org/10.1007/s10443-013-9347-2

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Skin Stringer Debonding Evolution in Stiffened Composite Panels under Compressive Load: A Novel Numerical Approach

Autor: A. Raimondo, Aniello Riccio, F. Scaramuzzino

Publikováno v: Key Engineering Materials. :605-608

In this paper, a numerical study, on the compressive behaviour of stiffened composite panels with skin-stringer debonding has been carried out. The analysis has been performed by adopting a novel robust (mesh and time step independent) finite element

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::03e8b9c14f92d4db9244b36c093c31bb
https://doi.org/10.4028/www.scientific.net/kem.577-578.605

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Impact Damage Management of Composite Laminated Structures by a Probabilistic Approach

Autor: Teresa Russo, Aniello Riccio, F. Scaramuzzino

Publikováno v: The Open Materials Science Journal. 7:8-22

A numerical procedure for the design of impact damage resistant composite laminated structures is proposed in the present paper. This procedure, based on probabilistic analyses, is able to support the design of complex composite laminated structures

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3df2f031f08e782bda9ec83ccdf17bc9
https://doi.org/10.2174/1874088x01307010008

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Stiffened panels damage tolerance determination using an optimization procedure based on a linear delamination growth approach

Autor: Andrea Sellitto, Francesco Di Caprio, Mauro Zarrelli, F. Scaramuzzino, Aniello Riccio

Publikováno v: American journal of science and engineering : 9 (2016): 1301–1317. doi:10.3844/ajeassp.2016.1301.1317
info:cnr-pdr/source/autori:Riccio A.; Di Caprio F.; Scaramuzzino F.; Sellitto A.; Zarrelli M./titolo:Stiffened panels damage tolerance determination using an optimization procedure based on a linear delamination growth approach/doi:10.3844%2Fajeassp.2016.1301.1317/rivista:American journal of science and engineering :/anno:2016/pagina_da:1301/pagina_a:1317/intervallo_pagine:1301–1317/volume:9

The damage tolerance of delaminated composite panels under compressive load is usually numerically evaluated by means of computationally expensive non-linear approaches. In this study, an alternative numerical linear approach, able to mimic the delam

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b991225cac01829bfc7739103f229e80
http://hdl.handle.net/11591/374136

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