MATEC Web Conf.
Volume 188, 20185th International Conference of Engineering Against Failure (ICEAF-V 2018)
|Number of page(s)||7|
|Section||Metallic Materials I: Characterization, Fatigue, Fracture and Fracture Mechanisms|
|Published online||07 August 2018|
Shear failure of AA2024 and AA7175 under high strain rate loading
Universitè de Toulouse, ISAE-SUPAERO, ICA (CNRS 5312),
2 National Defense University of Malaysia, Kuala Lumpur, Malaysia
* Corresponding author: firstname.lastname@example.org
In the context of the design of aeronautical structures regarding accidental events, we are here investigating and comparing the shear failure of two aluminum alloys, namely AA2024 and AA7175, under high strain rate loading. With this aim in view, two experiments were carried out: (i) high strain rate shear compression of hat shaped structures, and (ii) impact test on the edge of double notched plates. The fractured surfaces of post-mortem specimens were observed using optical and scanning electron microscopes (SEM) in order to identify the failure mechanisms.
© The Authors, published by EDP Sciences, 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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