Abstract
For the investigation of the creep-fatigue behaviour of X6 CrNi 1811 (similar to AISI Type 304 SS) sequential creep-fatigue tests, fatigue hold time experiments as well as fatigue relaxation tests have been performed and evaluated by different life-time prediction methods. The linear damage accumulation rule gave a satisfactory description only for a limited range of experimental parameters. First results for an extrapolation to 240h tension hold time indicate that, compared with the results of other life-time prediction methods, the linear damage accumulation rule appears to be a suitable tool for design purposes.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
