Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications

Delamination propagation in laminated composite materials is a common issue that always concerns us when we consider composites for structural purpose. Many possible solutions have been studied; the most famous is the three-dimensional (3D) woven composites materials, which have promising interlamin...

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Autores principales: Gaona Tiburcio, Citlalli, Lira Martínez, Manuel Alejandro, Gómez Avila, Marianggy, Jáquez Muñoz, Jesús Manuel, Baltazar Zamora, Miguel Ángel, Landa Ruiz, Laura, Nieves Mendoza, Demetrio, Estupiñan López, Francisco Humberto, Almeraya Calderón, Facundo
Formato: Sección de libro.
Lenguaje:inglés
Publicado: Intechopen 2023
Materias:
Acceso en línea:http://eprints.uanl.mx/25338/2/25338.pdf
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author Gaona Tiburcio, Citlalli
Lira Martínez, Manuel Alejandro
Gómez Avila, Marianggy
Jáquez Muñoz, Jesús Manuel
Baltazar Zamora, Miguel Ángel
Landa Ruiz, Laura
Nieves Mendoza, Demetrio
Estupiñan López, Francisco Humberto
Almeraya Calderón, Facundo
author_facet Gaona Tiburcio, Citlalli
Lira Martínez, Manuel Alejandro
Gómez Avila, Marianggy
Jáquez Muñoz, Jesús Manuel
Baltazar Zamora, Miguel Ángel
Landa Ruiz, Laura
Nieves Mendoza, Demetrio
Estupiñan López, Francisco Humberto
Almeraya Calderón, Facundo
author_sort Gaona Tiburcio, Citlalli
collection Repositorio Institucional
description Delamination propagation in laminated composite materials is a common issue that always concerns us when we consider composites for structural purpose. Many possible solutions have been studied; the most famous is the three-dimensional (3D) woven composites materials, which have promising interlaminar fracture resistance but at the cost of increasing density, which for aerospace industry is very important. In this chapter, mode 1 double cantilever beam (DCB) interlaminar fracture toughness tests according to the American Society for Testing and Materials (ASTM) D5528 standard were performed on composite specimens made of E-Glass Saertex 830 g/m2 Biaxial (+/−45°) with Sypol 8086 CCP polyester resin with orthogonal z-axis oriented yarn woven of 0.22 mm diameter nylon monofilament. Four specimens were made with a longitudinal distance between the warp binders of 0.5, 1, 1.5, and 2 cm, respectively. A tensile test according to the ASTM D3039 standard was performed to study how z-binder may affect tensile resistance. The results show a considerable increase in interlaminar fracture toughness, several stress concentrators have been created because of the new yarn and premature failure in the matrix.
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spelling eprints-253382025-07-03T14:27:33Z http://eprints.uanl.mx/25338/ Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications Gaona Tiburcio, Citlalli Lira Martínez, Manuel Alejandro Gómez Avila, Marianggy Jáquez Muñoz, Jesús Manuel Baltazar Zamora, Miguel Ángel Landa Ruiz, Laura Nieves Mendoza, Demetrio Estupiñan López, Francisco Humberto Almeraya Calderón, Facundo TA Ingeniería General y Civil Delamination propagation in laminated composite materials is a common issue that always concerns us when we consider composites for structural purpose. Many possible solutions have been studied; the most famous is the three-dimensional (3D) woven composites materials, which have promising interlaminar fracture resistance but at the cost of increasing density, which for aerospace industry is very important. In this chapter, mode 1 double cantilever beam (DCB) interlaminar fracture toughness tests according to the American Society for Testing and Materials (ASTM) D5528 standard were performed on composite specimens made of E-Glass Saertex 830 g/m2 Biaxial (+/−45°) with Sypol 8086 CCP polyester resin with orthogonal z-axis oriented yarn woven of 0.22 mm diameter nylon monofilament. Four specimens were made with a longitudinal distance between the warp binders of 0.5, 1, 1.5, and 2 cm, respectively. A tensile test according to the ASTM D3039 standard was performed to study how z-binder may affect tensile resistance. The results show a considerable increase in interlaminar fracture toughness, several stress concentrators have been created because of the new yarn and premature failure in the matrix. Intechopen 2023-03-29 Sección de libro. PeerReviewed text en cc_by_nc_nd http://eprints.uanl.mx/25338/2/25338.pdf http://eprints.uanl.mx/25338/2.haspreviewThumbnailVersion/25338.pdf Gaona Tiburcio, Citlalli y Lira Martínez, Manuel Alejandro y Gómez Avila, Marianggy y Jáquez Muñoz, Jesús Manuel y Baltazar Zamora, Miguel Ángel y Landa Ruiz, Laura y Nieves Mendoza, Demetrio y Estupiñan López, Francisco Humberto y Almeraya Calderón, Facundo (2023) Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications. In: Next generation fiber-reinforced composites. Intechopen, p. 24. ISBN 9781803569222 https://www.intechopen.com/books/11817
spellingShingle TA Ingeniería General y Civil
Gaona Tiburcio, Citlalli
Lira Martínez, Manuel Alejandro
Gómez Avila, Marianggy
Jáquez Muñoz, Jesús Manuel
Baltazar Zamora, Miguel Ángel
Landa Ruiz, Laura
Nieves Mendoza, Demetrio
Estupiñan López, Francisco Humberto
Almeraya Calderón, Facundo
Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications
thumbnail https://rediab.uanl.mx/themes/sandal5/images/online.png
title Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications
title_full Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications
title_fullStr Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications
title_full_unstemmed Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications
title_short Delamination and tensile effect of fine z-binder reinforced on fiberglass/polyester composite for aerospace applications
title_sort delamination and tensile effect of fine z binder reinforced on fiberglass polyester composite for aerospace applications
topic TA Ingeniería General y Civil
url http://eprints.uanl.mx/25338/2/25338.pdf
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