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...
Autores principales: | , , , , , , , , |
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Formato: | Sección de libro. |
Lenguaje: | inglés |
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Intechopen
2023
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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. |
format | Sección de libro. |
id | eprints-25338 |
institution | UANL |
language | English |
publishDate | 2023 |
publisher | Intechopen |
record_format | eprints |
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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