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Comparing Compression Deformation and Rate Sensitivity of Additively Manufactured and Extruded-Annealed 316L Alloys

  • Samed Enser
  • , Hakan Yavas*
  • , Burcu Arslan Hamat
  • , Hüseyin Aydın
  • , Gülten Kafadar
  • , A. Alptuğ Tanrıkulu
  • , Havva Zeytin Kazdal
  • , Fahrettin Ozturk
  • , Mustafa Güden
  • *Bu çalışma için yazışmadan sorumlu yazar
  • Izmir Institute of Technology
  • Turkish Aerospace Industries
  • Scientific and Technological Research Council of Turkey
  • Yildirim Beyazit Universitesi

Araştırma sonucu: Dergiye katkıMakalebilirkişi

8 Atıf (Scopus)

Özet

The deformation behavior of a selective-laser-melt-processed 316-L alloy (SLM-316L) under compression was determined together with a commercial annealed-extruded 316L alloy bar (C-316L) for comparison. Strain rate jump tests and hardness tests on the untested and compression tested samples were also performed. Extensive microscopic observations on the deformed and undeformed samples showed a twinning-dominated deformation in SLM-316L, similar to twinning-induced-plasticity steels, while a martensitic transformation-dominated deformation in C-316L alloy, similar to transformation-induced-plasticity steels. Within the studied quasi-static strain rate regime, the measured higher strain rate sensitivity of SLM-316L was ascribed to the lower distances between the nano-twins, in the level of 100 nm, than the distances between martensite plates, in the level of 1000 nm. A higher hardness increase in the martensite transformation region as compared with the twinned region proved the higher work hardening of C-316L. The hardness tests in the micron and sub-micron levels further confirmed the previously determined relatively low resistances of the dislocation cell walls (sub-grain) to the dislocation motion in SLM-316L alloy.

Orijinal dilİngilizce
Sayfa (başlangıç-bitiş)8831-8840
Sayfa sayısı10
DergiJournal of Materials Engineering and Performance
Hacim30
Basın numarası12
DOI'lar
Yayın durumuYayınlandı - Ara 2021
Harici olarak yayınlandıEvet

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Publisher Copyright:
© 2021, ASM International.

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