High Temperature Low Cycle Fatigue Properties and Failure Mechanism of a TiAl Alloy
Total strain range controlled low cycle fatigue (LCF) experiments were conducted at 750 ℃ to investigate the effects of the duplex and fully lamellar microstructure on fatigue behavior and life of a TiAl alloy, and the total strain range-life equation was employed to predict LCF life of the alloy. T...
Main Authors: | , , , , |
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Format: | Article |
Language: | zho |
Published: |
Journal of Aeronautical Materials
2017-10-01
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Series: | Journal of Aeronautical Materials |
Subjects: | |
Online Access: | http://jam.biam.ac.cn/CN/Y2017/V37/I5/77 |