Abstract
Alloy 617’s resistance to creep, fatigue and oxidation damage makes it suitable for structural applications at high temperatures (800-1000°C). Existing experimental techniques for investigating the creep-fatigue response use strain-based cyclic loading with a dwell time to generate varying portions of fatigue and creep damage respectively. Due to rapid stress relaxation of Alloy 617 at high temperatures, strain-based creep-fatigue testing only generates fatigue-dominant damage. Tests that produce creep-dominant damage are therefore essential to fully understand the creep-fatigue interaction for this alloy. Designing creep-dominant creep-fatigue tests is a challenging task due to large inelastic strains produced at high temperatures. Thus, multiple testing profiles must be examined to achieve this goal. This paper presents the stress-strain curves and experimental observations for various testing profiles and also discusses the microstructural aspects of the failed specimens. The authors propose a new loading profile that produces a larger fraction of creep damage thereby completing the failure envelope of Alloy 617 on a creep-fatigue interaction diagram.
Original language | English (US) |
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Title of host publication | 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624103926 |
State | Published - 2016 |
Event | 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016 - San Diego, United States Duration: Jan 4 2016 → Jan 8 2016 |
Other
Other | 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016 |
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Country/Territory | United States |
City | San Diego |
Period | 1/4/16 → 1/8/16 |
ASJC Scopus subject areas
- Civil and Structural Engineering
- Building and Construction
- Architecture
- Mechanics of Materials