Proposal of estimation method for notched specimen fatigue limit of commercially pure titanium

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In order to identify the fatigue limit for a sharp notched specimen of commercially pure titanium, rotating bending fatigue tests on smooth and notched specimens were curried out. In previous studies, it was found that the fatigue limit for a sharp notched specimen of commercially pure titanium could not be determined and it is not sure whether it fail over N=10 7 cycles or not. Based on the experimental results, in the smooth specimen and notched specimen (p=1.0mm), they have fatigue limits and knee points, while the sharp notched specimen (p=0.1mm) does not. As an estimation method, the fatigue crack initiation of each specimen was then investigated. The investigation results are as follows. (1) The proportional relationship exists between the maximum stress K iωa at the notch root and logarithm of the number of cycles to fatigue crack initiation N i. (2) Based on the slope of the relationship between the maximum stress K iωa and the number of cycles to fatigue crack initiation N i at the notch root, there is no possibility that the fatigue crack in the same mechanism initiates over N=10 7 cycles. Therefore, the stress amplitude that is not initiated the fatigue crack at N=10 7 cycles is the fatigue limit.

Original languageEnglish
Title of host publication17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures
Pages937-944
Number of pages8
Volume2
Publication statusPublished - 2008
Event17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures, ECF17 - Brno, Czech Republic
Duration: Sep 2 2008Sep 5 2008

Other

Other17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures, ECF17
CountryCzech Republic
CityBrno
Period9/2/089/5/08

Fingerprint

Titanium
Fatigue of materials
Crack initiation
Fatigue cracks

All Science Journal Classification (ASJC) codes

  • Civil and Structural Engineering

Cite this

Fujii, T., Hamada, S., & Noguchi, H. (2008). Proposal of estimation method for notched specimen fatigue limit of commercially pure titanium. In 17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures (Vol. 2, pp. 937-944)

Proposal of estimation method for notched specimen fatigue limit of commercially pure titanium. / Fujii, Takumi; Hamada, Shigeru; Noguchi, Hiroshi.

17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures. Vol. 2 2008. p. 937-944.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fujii, T, Hamada, S & Noguchi, H 2008, Proposal of estimation method for notched specimen fatigue limit of commercially pure titanium. in 17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures. vol. 2, pp. 937-944, 17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures, ECF17, Brno, Czech Republic, 9/2/08.
Fujii T, Hamada S, Noguchi H. Proposal of estimation method for notched specimen fatigue limit of commercially pure titanium. In 17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures. Vol. 2. 2008. p. 937-944
Fujii, Takumi ; Hamada, Shigeru ; Noguchi, Hiroshi. / Proposal of estimation method for notched specimen fatigue limit of commercially pure titanium. 17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures. Vol. 2 2008. pp. 937-944
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