Testing and simulation of a composite-aluminium wingbox subcomponent subjected to thermal loading

Autor: Jordi Llobet Vallejo, Josep Costa Balanzat, Jose Manuel Guerrero, Aravind Sasikumar

Publikováno v: Composite Structures, 2022, vol. 296, art.núm. 115887
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DUGiDocs – Universitat de Girona
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Modern aircraft designs combine carbon–aluminium assemblies mechanically joined by steel bolts. The different thermal expansion coefficient of these materials and the substantial temperature excursions during aircraft operation, lead to thermal str

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2f7c7042809fa763071c8013031cee8b
https://doi.org/10.1016/j.compstruct.2022.115887

Experimental study into compression after impact strength of laminates with conventional and nonconventional ply orientations

Autor: Emilio Vicente González, Lorena Marín, Josep Costa Balanzat, Yi Liv, AMADE AMADE, Joan Andreu Mayugo, Gerard Guillamet

Publikováno v: Recercat. Dipósit de la Recerca de Catalunya
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© Composites Part B: Engineering, 2017, vol. 126, p. 133-142
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DUGiDocs – Universitat de Girona

The quest for impact damage tolerant laminates by tailoring stacking sequences has led to nonconventional laminates whose ply sequences are not limited to 0, ±45 and 90°. Departing from the hypothesis that compression after impact (CAI) strength is

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6a6e5ecd971d202d80e1db3dcf11af3e
https://doi.org/10.1016/j.compositesb.2017.05.074

An experimental data reduction method for the Mixed Mode Bending test based on the J-integral approach

Autor: Carlos Sarrado, Josep Costa Balanzat, Jordi Renart, AMADE AMADE, Albert Turon

Publikováno v: © Composites Science and Technology, 2015, vol. 117, p. 85-91
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DUGiDocs – Universitat de Girona
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The Mixed Mode Bending test (MMB) is suitable for measuring the interlaminar fracture toughness of composite materials under mixed-mode loading. Data reduction is usually based on the assumptions of Linear Elastic Fracture Mechanics, which are not fu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2cfdf50234a3e1074213ffe4c6941efc
https://doi.org/10.1016/j.compscitech.2015.05.021

Damage resistance and damage tolerance of dispersed CFRP laminates: Effect of the mismatch angle between plies

Autor: Tamer Sebaey, Emilio Vicente González, Josep Costa Balanzat, Norbert Blanco, AMADE AMADE, Cláudio Lopes, Pere Maimí

Publikováno v: Composite Structures. 101:255-264

Damage resistance and damage tolerance to impact events is the most demanding criteria in sizing several aeronautical composites. Tailoring the laminate ply sequence represents an effort towards improving those properties. In this work, the effect of

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::405f6af82a6444a5d440b973fbd7b5b5
https://doi.org/10.1016/j.compstruct.2013.01.026

A quasi-static indentation test to elucidate the sequence of damage events in low velocity impacts on composite laminates

Autor: Josep Costa Balanzat, Norbert Blanco, AMADE AMADE, Ahmed Wagih, Pere Maimí

Publikováno v: © Composites Part A: Applied Science and Manufacturing, 2016, vol. 82, p. 180-189
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DUGiDocs – Universitat de Girona
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Any attempt to achieve composite laminates with improved damage tolerance to low velocity impacts must depart from the understanding of the sequence of damage mechanisms taking place. To this purpose, a series of quasi-static indentation experiments

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6ed05d6290b22427df718a8093534212
http://hdl.handle.net/10256/12369