Loading sequence effect on fatigue life of Type 316 stainless steel

Kamaya, Masayuki; Kawakubo, Masahiro

doi:10.1016/j.ijfatigue.2015.07.009

Cited by 43 publications

(32 citation statements)

References 57 publications

(95 reference statements)

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“…Some of the setups include a disc heated by induction on the periphery [1][2][3][4][5][6][7][8][9][10][11][12], triangular blade heated by induction [13], electrical heating of tube followed by water splashing to induce thermal shock [14][15][16][17][18], hot dipping of cylinders in molten aluminum [19,20], laser heating [21,22], focused halogen lamps heating [23,24], convection/combustion heating [25,26], furnace heating with water quenching [27,28] and actual dies [29,30]. Out of these experimental setups most researchers have worked on the heated disc problem.…”

Section: Introductionmentioning

confidence: 99%

Numerical simulation of thermal fatigue behavior in a cracked disc of AISI H-11 tool steel

Qayyum

Shah

Shakeel

et al. 2016

Engineering Failure Analysis

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Section: Introductionmentioning

confidence: 99%

Numerical simulation of thermal fatigue behavior in a cracked disc of AISI H-11 tool steel

Qayyum

Shah

Shakeel

et al. 2016

Engineering Failure Analysis

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“…In addition, the experimental results of other materials, including Ti‐6Al‐4V, Al‐2024‐T42, 30CrMnSiA, 30NiCrMoV12, NiTi, GS61, ENAW6005, P335NL1, and 316 Steel, were utilized to validate the application of the proposed model. The tests results of the aforementioned materials under LH block loadings were listed in Table .…”

Section: Resultsmentioning

confidence: 99%

“…The predicted lives versus the experimental results of different materials [Colour figure can be viewed at wileyonlinelibrary.com]…”

Section: Resultsmentioning

confidence: 99%

“…Palmgren‐Miner rule, a linear fatigue damage accumulation model, was first proposed to estimate the accumulated fatigue damage in 1945. However, the linear damage accumulation rule would result in an overestimated fatigue life in the case of HL block loading and a shorter predicted fatigue life in the LH loading path . To overcome this shortcoming, numerous nonlinear cumulative fatigue damage models had been proposed considering the influence of loading history .…”

Section: Introductionmentioning

confidence: 99%

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Residual fatigue life prediction based on a novel damage accumulation model considering loading history

Shi

et al. 2020

Fatigue Fract Eng Mat Struct

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The influence of prior low‐cycle fatigue (LCF) on the residual fatigue life was investigated experimentally. A Ni‐based alloy was cyclically loaded under stress‐controlled low‐high (LH) block loading. In the first loading step, low‐amplitude loading was performed with the stress amplitude of 283.5MPa at 710°C. Different cycles of preloading were performed, varying from 100 to 10 000. Subsequently, high‐amplitude fatigue loading was carried out with the stress amplitude of 315MPa at 800°C. Experimental results show that the previous loading was beneficial to the residual fatigue life when the consumed life fraction is below 0.2 and detrimental when the consumed life fraction is larger than 0.2. A novel nonlinear fatigue damage accumulation model was proposed to estimate the residual LCF life under LH loading path considering the effects of load sequence and preloading cycles. The proposed model provided a better life prediction than some existing models, such as Kwofie‐Rahbar model, Miner' rule, Peng model, and Ye‐Wang model. Lastly, this model was further validated using various materials under LH and high‐low block loadings.

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“…(III) Crack opening displacement: Positron annihilation could occur in the opening space of the crack wake. In terms of the factor (I), some strain‐controlled low cycle fatigue tests of type 316, in which strain amplitudes were ranging from 0.2 to 1%, revealed that the cyclic stress responses stabilized due to work hardening at the early stage of fatigue lives. For example, the stress‐strain response was stabilized at about 1% of total fatigue life at the strain amplitude of 0.2% by Kamaya and Kawakubo, and at about 20% of total fatigue life at the amplitude of 0.3% by Roya et al …”

Section: Resultsmentioning

confidence: 99%

Non‐destructive evaluation of fatigue damage and fatigue crack initiation in type 316 stainless steel by positron annihilation line‐shape and lifetime analyses

Uematsu

Kakiuchi

Hattori

et al. 2016

Fatigue Fract Eng Mat Struct

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Rotating bending fatigue tests were conducted using type 316 stainless steel. The fatigue tests were periodically terminated, and fatigue damage and fatigue crack initiation were non‐destructively and sequentially evaluated by positron annihilation line‐shape and lifetime analyses. The counter‐jig and anticoincidence methods were used for positron annihilation line‐shape and lifetime analyses, respectively, to enhance the analytical precision. The fatigue crack lengths were monitored by a plastic replication technique, and related to the parameters in both analyses. S‐parameter obtained in the line‐shape analysis increased with increasing fatigue damage, while it was difficult to detect fatigue crack initiation and subsequent small fatigue crack growth. That was because the precision of line‐shape analysis was limited. On the other hand, both fatigue damage and fatigue crack initiation were successfully detected by lifetime analysis. Positron annihilation lifetime also increased with increasing fatigue damage, and lifetime was longer at the notch root with fatigue crack than at the smooth section without crack. It was considered that the precision of lifetime analysis was high enough to detect high dislocation density areas at the fatigue crack tips.

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Loading sequence effect on fatigue life of Type 316 stainless steel

Cited by 43 publications

References 57 publications

Numerical simulation of thermal fatigue behavior in a cracked disc of AISI H-11 tool steel

Numerical simulation of thermal fatigue behavior in a cracked disc of AISI H-11 tool steel

Residual fatigue life prediction based on a novel damage accumulation model considering loading history

Non‐destructive evaluation of fatigue damage and fatigue crack initiation in type 316 stainless steel by positron annihilation line‐shape and lifetime analyses

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