Analysis of testing at high strain rates using FEM

Caballero Herranz, Jesús

Publication:
Analysis of testing at high strain rates using FEM

dc.contributor.advisor	Pernas Sánchez, Jesús
dc.contributor.advisor	Artero Guerrero, José Alfonso
dc.contributor.author	Caballero Herranz, Jesús
dc.contributor.departamento	UC3M. Departamento de Mecánica de Medios Continuos y Teoría de Estructuras	es
dc.date.accessioned	2021-01-12T11:47:07Z
dc.date.available	2021-01-12T11:47:07Z
dc.date.issued	2020-03
dc.date.submitted	2020-03-12
dc.description.abstract	The use of composite materials in aviation is increasing every year. They offer huge advantages in terms of performance and weight with respect to more common materials such as aluminum. However, the sector of aviation is both very conservative and progressive at the same time. They invest a lot of time and money in developing new, more efficient ways of operating, but also take a lot of time to introduce these improvements into the market. This is, of course, due to safety reasons. A fatal error taking place during flight can be catastrophic. For this reason it is important to perform thorough tests in new materials introduced. The simulation using a FEM software of a SHPB experiment is a great way of testing the materials at the high strain rates it could encounter during operation. Therefore, seeing that the proposed material passes the test satisfactorily, its introduction into the industry can be approved. The validation of these experiments using FEM software is reached when the results obtained match the characteristics of the materials tested, which are already known. This has great value for the industry as these simulations allow to test a wide variety of materials in many different configurations and could help reduce time and cost.	es
dc.description.degree	Ingeniería Aeroespacial	es
dc.identifier.uri	https://hdl.handle.net/10016/31681
dc.language.iso	eng	es
dc.rights	Atribución-NoComercial-SinDerivadas 3.0 España	*
dc.rights.accessRights	open access	es
dc.rights.uri	http://creativecommons.org/licenses/by-nc-nd/3.0/es/	*
dc.subject.eciencia	Aeronáutica	es
dc.subject.eciencia	Materiales	es
dc.subject.other	FEM	es
dc.subject.other	Split Hopkinson Pressure Bar	es
dc.subject.other	SHPB	es
dc.subject.other	Composite materials	es
dc.subject.other	High strain rate	es
dc.subject.other	Unidirectional CRFP	es
dc.subject.other	Aviation	es
dc.title	Analysis of testing at high strain rates using FEM	es
dc.type	bachelor thesis	*
dspace.entity.type	Publication