Analysis of testing at high strain rates using FEM

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dc.contributor.advisor Pernas Sánchez, Jesús
dc.contributor.advisor Artero Guerrero, José Alfonso
dc.contributor.author Caballero Herranz, Jesús
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.identifier.uri http://hdl.handle.net/10016/31681
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.
dc.language.iso eng
dc.rights Atribución-NoComercial-SinDerivadas 3.0 España
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject.other FEM
dc.subject.other Split Hopkinson Pressure Bar
dc.subject.other SHPB
dc.subject.other Composite materials
dc.subject.other High strain rate
dc.subject.other Unidirectional CRFP
dc.subject.other Aviation
dc.title Analysis of testing at high strain rates using FEM
dc.type bachelorThesis
dc.subject.eciencia Aeronáutica
dc.subject.eciencia Materiales
dc.rights.accessRights openAccess
dc.description.degree Ingeniería Aeroespacial
dc.contributor.departamento Universidad Carlos III de Madrid. Departamento de Mecánica de Medios Continuos y Teoría de Estructuras
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