Effect of forging process on high cycle and very high cycle fatigue properties of TC4 titanium alloy under three‐point bending
The ultrasonic fatigue tests under two three‐point bending loading modes were carried out on TC4 specimens with the equiaxed, bimodal, and lamellar microstructure in the range of 105 to 109 cycles. The S‐N curves with different shapes were obtained, and it was found that the crack initiation in very...
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Published in | Fatigue & fracture of engineering materials & structures Vol. 44; no. 8; pp. 2054 - 2069 |
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Main Authors | , , , , , |
Format | Journal Article |
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01.08.2021
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Abstract | The ultrasonic fatigue tests under two three‐point bending loading modes were carried out on TC4 specimens with the equiaxed, bimodal, and lamellar microstructure in the range of 105 to 109 cycles. The S‐N curves with different shapes were obtained, and it was found that the crack initiation in very high cycle regime changed from surface to subsurface. The crack initiation mechanism with different microstructures was revealed by fracture analysis. The axial tension influence mechanism is that it changes the axial stress distribution on the specimen cross section and makes the crack origin migrate to the interior. |
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AbstractList | The ultrasonic fatigue tests under two three‐point bending loading modes were carried out on TC4 specimens with the equiaxed, bimodal, and lamellar microstructure in the range of 105 to 109 cycles. The S‐N curves with different shapes were obtained, and it was found that the crack initiation in very high cycle regime changed from surface to subsurface. The crack initiation mechanism with different microstructures was revealed by fracture analysis. The axial tension influence mechanism is that it changes the axial stress distribution on the specimen cross section and makes the crack origin migrate to the interior. Abstract The ultrasonic fatigue tests under two three‐point bending loading modes were carried out on TC4 specimens with the equiaxed, bimodal, and lamellar microstructure in the range of 10 5 to 10 9 cycles. The S ‐ N curves with different shapes were obtained, and it was found that the crack initiation in very high cycle regime changed from surface to subsurface. The crack initiation mechanism with different microstructures was revealed by fracture analysis. The axial tension influence mechanism is that it changes the axial stress distribution on the specimen cross section and makes the crack origin migrate to the interior. |
Author | Wang, Bohan Li, Dongchun Cui, Wenbin Wang, Changkai Cheng, Li Chen, Xuan |
Author_xml | – sequence: 1 givenname: Bohan orcidid: 0000-0003-2424-1880 surname: Wang fullname: Wang, Bohan email: dream0729ing@foxmail.com organization: Air Force Engineering University – sequence: 2 givenname: Li surname: Cheng fullname: Cheng, Li organization: Air Force Engineering University – sequence: 3 givenname: Wenbin surname: Cui fullname: Cui, Wenbin organization: Air Force Engineering University – sequence: 4 givenname: Xuan surname: Chen fullname: Chen, Xuan organization: Air Force Engineering University – sequence: 5 givenname: Changkai surname: Wang fullname: Wang, Changkai organization: Air Force Engineering University – sequence: 6 givenname: Dongchun surname: Li fullname: Li, Dongchun organization: Air Force Engineering University |
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Snippet | The ultrasonic fatigue tests under two three‐point bending loading modes were carried out on TC4 specimens with the equiaxed, bimodal, and lamellar... Abstract The ultrasonic fatigue tests under two three‐point bending loading modes were carried out on TC4 specimens with the equiaxed, bimodal, and lamellar... |
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SubjectTerms | Axial stress Bending fatigue combined loading Crack initiation fatigue crack initiation Fatigue tests Forging Fracture mechanics fracture morphology High cycle fatigue Stress concentration Stress distribution titanium alloy Titanium alloys Titanium base alloys very high cycle fatigue |
Title | Effect of forging process on high cycle and very high cycle fatigue properties of TC4 titanium alloy under three‐point bending |
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