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Numerical study of the impact response and ballistic limit of AA2024 friction stir welded aircraft panels

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Numerical study of the impact response and ballistic limit of AA2024 friction stir welded aircraft panels

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Azorín Albero, A. (2014). Numerical study of the impact response and ballistic limit of AA2024 friction stir welded aircraft panels. Universitat Politècnica de València. http://hdl.handle.net/10251/51049

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Title: Numerical study of the impact response and ballistic limit of AA2024 friction stir welded aircraft panels
Author: Azorín Albero, Adrián
Director(s): Tom de Vuyst
UPV Unit: Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny
Read date / Event date:
2014-09
Issued date:
Abstract:
Friction Stir Welding is a novel environmentally friendly welding technique able to produce higher joint properties than conventional processes. It has become an attractive process for many manufacturers in the last years, ...[+]
Subjects: Hard projectile , Barlat’s material model , LS-DYNA , FSW , Anisotropy , Soft projectile , Residual velocity , SPH bird , Residual stresses
Copyrigths: Cerrado
Publisher:
Universitat Politècnica de València
degree: Máster Universitario en Ingeniería Aeronáutica-Màster Universitari en Enginyeria Aeronàutica
Type: Tesis de máster

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