Computing the durability of WAAM 18Ni 250 maraging steel specimens

Author:

Peng Daren12ORCID,Jones Rhys12ORCID,Ang Andrew S. M.1,Michelson Alex3,Champagne Victor4,Birt Aaron3,Pinches Samuel1,Kundu Sudip25,Alankar Alankar5,Singh Raman R. K.2

Affiliation:

1. ARC Training Centre on Surface Engineering for Advanced Materials (SEAM), School of Engineering Swinburne University of Technology Hawthorn Victoria Australia

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

3. Solvus Global Worcester Massachusetts USA

4. US Army Research Laboratory U.S. Army Combat Capabilities Development Command Weapons and Materials Research Directorate Aberdeen Maryland USA

5. Department of Mechanical Engineering Indian Institute of Technology Bombay Mumbai Maharashtra India

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference52 articles.

1. Additively manufactured Ti-6Al-4V replacement parts for military aircraft

2. US army directive 2019‐29 enabling readiness and modernization through advanced manufacturing. Secretary of The Army Pentagon Washington DC 18th September 2019. Accessed February 07 2022.https://armypubs.army.mil/epubs/DR_pubs/DR_a/pdf/web/ARN19451_AD2019-29_Web_Final.pdf

3. Structures Bulletin EZ‐SB‐19‐01 durability and damage tolerance certification for additive manufacturing of aircraft structural metallic parts. Wright Patterson Air Force Base OH USA 10 June2019. Accessed February 07 2022.https://daytonaero.com/usaf-structures-bulletins-library/

4. Department of Defense Joint Service Specification Guide aircraft structures JSSG‐2006 October1998. Accessed February 07 2022. Available online at:http://everyspec.com/USAF/USAF-General/JSSG-2006_10206/

5. MIL‐STD‐1530D Department Of Defense Standard Practice Aircraft Structural Integrity Program (ASIP) 13 October2016. Accessed February 07 2022. Available online athttp://everyspec.com/MIL‐STD/MIL‐STD.../download.php?spec=MIL‐STD‐1530D

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