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Further Studies into Crack Growth in Additively Manufactured Materials.

ABSTRACT: Understanding and characterizing crack growth is central to meeting the damage tolerance and durability requirements delineated in USAF Structures Bulletin EZ-SB-19-01 for the utilization of additive manufacturing (AM) in the sustainment of aging aircraft. In this context, the present paper discusses the effect of different AM processes, different build directions, and the variability in the crack growth rates related to AM Ti-6Al-4V, AM Inconel 625, and AM 17-4 PH stainless steel. This study reveals that crack growth in these three AM materials can be captured using the Hartman-Schijve crack growth equation and that the variability in the various da/dN versus ?K curves can be modeled by allowing the terms ?Kthr and A to vary. It is also shown that for the AM Ti-6AL-4V processes considered, the variability in the cyclic fracture toughness appears to be greatest for specimens manufactured using selective layer melting (SLM).

SUBMITTER: Iliopoulos AP

PROVIDER: S-EPMC7287604 | biostudies-literature | 2020 May

REPOSITORIES: biostudies-literature

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Further Studies into Crack Growth in Additively Manufactured Materials.

Iliopoulos Athanasios P AP Jones Rhys R Michopoulos John G JG Phan Nam N Rans Calvin C

Materials (Basel, Switzerland) 20200512 10

Understanding and characterizing crack growth is central to meeting the damage tolerance and durability requirements delineated in USAF Structures Bulletin EZ-SB-19-01 for the utilization of additive manufacturing (AM) in the sustainment of aging aircraft. In this context, the present paper discusses the effect of different AM processes, different build directions, and the variability in the crack growth rates related to AM Ti-6Al-4V, AM Inconel 625, and AM 17-4 PH stainless steel. This study re ...[more]

PMID: 32408649

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