Experimental Investigation of High-temperature Crack Propagation Behaviors for Ti-6Al-4V/ELI at 250 <b>℃</b>
Fatigue crack propagation behaviors at high temperature are important preconditions for damage tolerance design in aircraft and engine structures.Therefore, fatigue tests were carried out on titanium alloy Ti-6Al-4V/ELI subjected to constant amplitude loading at two temperatures of 25 ℃ and 250 ℃ an...
Main Authors: | , , , |
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Format: | Article |
Language: | zho |
Published: |
Journal of Aeronautical Materials
2018-08-01
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Series: | Journal of Aeronautical Materials |
Subjects: | |
Online Access: | http://jam.biam.ac.cn/CN/Y2018/V38/I4/123 |