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: | LYU Zhiyang, XIONG Junjiang, ZHAO Yanguang, MA Shaojun |
---|---|
Format: | Article |
Language: | zho |
Published: |
Journal of Aeronautical Materials
2018-08-01
|
Series: | Journal of Aeronautical Materials |
Subjects: | |
Online Access: | http://jam.biam.ac.cn/CN/Y2018/V38/I4/123 |
Similar Items
-
Impact of Cryogenic Treatment on HCF and FCP Performance of β-Solution Treated Ti-6Al-4V ELI Biomaterial
by: Anil Kumar Singla, et al.
Published: (2020-01-01) -
Effect of morphology of primary a on fatigue crack propagation resistance in a near a heat resistant Titanium alloy
by: Sumi Y., et al.
Published: (2020-01-01) -
Effect of TiB Orientation on Near-Threshold Fatigue Crack Propagation in TiB-Reinforced Ti-3Al-2.5V Matrix Composites Treated with Heat Extrusion
by: Shoichi Kikuchi, et al.
Published: (2019-11-01) -
Effect of Parameters on Fatigue Properties and Crack Propagation Behavior of Friction Stir Crack Repaired Al2024
by: Lei Wang, et al.
Published: (2020-07-01) -
Fatigue crack propagation in short-fiber reinforced plastics
by: K. Tanaka, et al.
Published: (2015-09-01)