Modelling Crack Growth in Additively Manufactured Inconel 718 and Inconel 625

Author:

Jones Rhys12ORCID,Ang Andrew1ORCID,Peng Daren12ORCID,Champagne Victor K.3,Michelson Alex4,Birt Aaron4

Affiliation:

1. ARC Industrial Transformation Training Centre on Surface Engineering for Advanced Materials, School of Engineering, Swinburne University of Technology, John Street, Hawthorn, VIC 3122, Australia

2. Centre of Expertise for Structural Mechanics, Department of Mechanical and Aerospace Engineering, Monash University, Clayton, VIC 3800, Australia

3. US Army Research Laboratory, U.S. Army Combat Capabilities Development Command Weapons and Materials Research Directorate, Aberdeen Proving Ground, Adelphi, MD 20783-1138, USA

4. Solvus Global, 104 Prescott Street, Worcester, MA 01605, USA

Abstract

This paper first examines crack growth in a range of tests on additively manufactured (AM) and conventionally manufactured Inconel 718. It is shown that whereas when the crack growth rate (da/dN) is plotted as a function of the range of the stress intensity factor (ΔK), the crack growth curves exhibit considerable scatter/variability, when da/dN is expressed in terms of the Schwalbe crack driving force (Δκ), then each of the 33 different curves essentially collapse onto a single curve. This relationship appears to hold over approximately six orders of magnitude in da/dN. The same phenomenon also appears to hold for 20 room temperature tests on both conventionally and additively manufactured Inconel 625. Given that the 53 studies examined in this paper were taken from a wide cross section of research studies it would appear that the variability in the da/dN and ΔK curves can (to a first approximation) be accounted for by allowing for the variability in the fatigue threshold and the cyclic fracture toughness terms in the Schwalbe crack driving force. As such, the materials science community is challenged to address the fundamental science underpinning this observation.

Funder

US Army International Technology Center, Indo-Pacific (ITC-IPAC), Tokyo

Publisher

MDPI AG

Subject

General Materials Science,Metals and Alloys

Reference63 articles.

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2. (1998). Joint Service Specification Guide, Aircraft Structures (Standard No. JSSG-2006).

3. (2021, August 02). NASA-HDBK-5010, Fracture Control Handbook for Payloads, Experiments, And Similar Hardware, May 2005, Revalidated 2012, Available online: https://standards.nasa.gov/standard/nasa/nasa-hdbk-5010.

4. (2019). Structures Bulletin. Durability and Damage Tolerance Certification for Additive Manufacturing of Aircraft Structural Metallic Parts (Standard No. EZ-SB-19-01).

5. Economic life determination for a military aircraft;Lincoln;J. Aircr.,1999

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