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An Experimental and Numerical Investigation to Characterize an Aerospace Composite Material with Open-Hole Using Non-Destructive Techniques

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An Experimental and Numerical Investigation to Characterize an Aerospace Composite Material with Open-Hole Using Non-Destructive Techniques

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Feito-Sánchez, N.; Calvo, JV.; Belda, R.; Giner Maravilla, E. (2020). An Experimental and Numerical Investigation to Characterize an Aerospace Composite Material with Open-Hole Using Non-Destructive Techniques. Sensors. 20(15):1-18. https://doi.org/10.3390/s20154148

Por favor, use este identificador para citar o enlazar este ítem: http://hdl.handle.net/10251/176339

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Title: An Experimental and Numerical Investigation to Characterize an Aerospace Composite Material with Open-Hole Using Non-Destructive Techniques
Author: Feito-Sánchez, Norberto Calvo, José Vicente Belda, R. Giner Maravilla, Eugenio
UPV Unit: Universitat Politècnica de València. Departamento de Ingeniería Mecánica y de Materiales - Departament d'Enginyeria Mecànica i de Materials
Issued date:
Abstract:
[EN] In this study, the open-hole quasi-static tensile and fatigue loading behavior of a multidirectional CFRP thick laminate, representative of laminates used in the aerospace industry, is studied. Non-destructive techniques ...[+]
Subjects: CFRP , Fatigue , Digital image correlation , Infrared thermography , Open hole
Copyrigths: Reconocimiento (by)
Source:
Sensors. (eissn: 1424-8220 )
DOI: 10.3390/s20154148
Publisher:
MDPI AG
Publisher version: https://doi.org/10.3390/s20154148
Project ID:
info:eu-repo/grantAgreement/AEI//DPI2017-89197-C2-1-R//TALADRADO DE COMPONENTES HIBRIDOS CFRPS/TI Y TOLERANCIA AL DAÑO DEBIDO A MECANIZADO DURANTE EL COMPORTAMIENTO EN SERVICIO DE UNIONES ESTRUCTURALES AERONAUTICAS/
info:eu-repo/grantAgreement/GVA//PROMETEO%2F2016%2F007//Modelado numérico avanzado en ingeniería mecánica/
info:eu-repo/grantAgreement/AEI//DPI2017-89197-C2-2-R-AR//TALADRADO DE COMPONENTES HIBRIDOS CFRPS/TI Y TOLERANCIA AL DAÑO DEBIDO A MECANIZADO DURANTE EL COMPORTAMIENTO EN SERVICIO DE UNIONES ESTRUCTURALES AERONAUTICAS/
Thanks:
This research was funded by the FEDER programme and the Spanish Ministerio de Ciencia, Innovacion y Universidades, projects DPI2017-89197-C2-1-R and DPI2017-89197-C2-2-R. The funding of the Generalitat Valenciana, Programme ...[+]
Type: Artículo

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