Results of a Pilot Study in Support of a Round-Robin on Creep-Fatigue Crack Growth Testing of a Creep-Brittle Material for ASTM E2760

Author:

Gibson Cody1,Stephens Robert1,Narasimhachary Santosh B.2,Mills David E.3,Rosenberger Andrew4

Affiliation:

1. Department of Mechanical Engineering, University of Idaho, 875 Perimeter Dr. MS 0902, Moscow, ID 83844-0902, USA

2. Siemens Technology, 5101 Westinghouse Blvd., Charlotte, NC 28273-9640, USA (Corresponding author), e-mail: Santosh.narasimhachary@siemens.com,https://orcid.org/0000-0002-8915-0237

3. Rolls-Royce Corporation, PO Box 420, MC-S6-04, Indianapolis, IN 46206, USA

4. Air Force Research Lab, 2230 Tenth St., Ste 1, Wright-Patterson AFB, OH 45433, USA

Publisher

ASTM International

Subject

Metals and Alloys,Polymers and Plastics,Mechanics of Materials,Ceramics and Composites

Reference12 articles.

1. An Investigation of Creep-Fatigue-Environment Interactions in Ni-Base Superalloy;Floreen;Fatigue & Fracture of Engineering Materials & Structures,1979

2. A. Saxena, “A Model for Predicting the Environment Enhanced Fatigue Crack Growth Behavior at High Temperature,” in Thermal and Environmental Effects in Fatigue: Research-Design Interface, eds. S. J. Hudak, M. E. Mayfield, and C. E. Jaske (New York: American Society of Mechanical Engineers, 1983), 171–184.

3. R. M. Pelloux and J. S. Huang, “Creep-Fatigue-Environment Interactions in Astrolloy,” in Creep-Fatigue Environment Interactions, eds. R. Pelloux and N. Stolloff (Warrendale, PA: TMS-AIME, 1980), 151–164.

4. Oxygen-Induced Intergranular Fracture of the Nickel-Base Alloy IN718 During Mechanical Loading at High Temperatures;Krupp;Materials Research,2004

5. Standard Test Method for Creep-Fatigue Crack Growth Testing, ASTM E2760-10e1 (West Conshohocken, PA: ASTM International, approved May 1, 2010), https://doi.org/10.1520/E2760-19E01

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