2014
DOI: 10.1007/s11223-014-9563-5
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Influence of Temperature on Fatigue Crack Propagation in TiAl Alloys*

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Cited by 5 publications
(6 citation statements)
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“…Stage II) is essential. FCG data of region II fatigue of Ti–48Al–2Mn–2Nb [19,20] shows that both the crack growth prefactor, , and the Paris slope, n , decrease significantly above 750C (the latter to n =4), suggesting that once the ductile–brittle transition is exceeded, damage-tolerant design may be achievable if sufficient strength can be maintained. It has been reported that the Paris slope is lower when the lamellae in a TiAl lamellar colony are oriented parallel to the loading axis [21].…”
Section: Conventional Macroscopic Analysis Of the Hcf Behaviour Of γ-...mentioning
confidence: 99%
“…Stage II) is essential. FCG data of region II fatigue of Ti–48Al–2Mn–2Nb [19,20] shows that both the crack growth prefactor, , and the Paris slope, n , decrease significantly above 750C (the latter to n =4), suggesting that once the ductile–brittle transition is exceeded, damage-tolerant design may be achievable if sufficient strength can be maintained. It has been reported that the Paris slope is lower when the lamellae in a TiAl lamellar colony are oriented parallel to the loading axis [21].…”
Section: Conventional Macroscopic Analysis Of the Hcf Behaviour Of γ-...mentioning
confidence: 99%
“…Apart from oxidation, the fatigue crack propagation rate is found to be stro fected by temperature. Feng et al [103] noted the increase in the fatigue crack gro in the temperature range of 25-750 °C. Nevertheless, when the temperature was 750 and 850 °C, the rate decreased.…”
Section: Microstructural Mechanismsmentioning
confidence: 97%
“…To take into account both stage It is noteworthy that the Paris model (Equation ( 3)) has been modified by several researchers to incorporate other important factors that significantly influence the FCGR of these intermetallic alloys. For instance, to reflect the influence of average stress on the crack propagation rate and to show the effects of accelerated crack propagation when the stress intensity factor ∆K approaches the critical value K IC , Forman [103] modified the Paris model as follows:…”
Section: Fatigue Crack Propagation Modelsmentioning
confidence: 99%
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“…Within this event, a special session named mechanical properties of materials was held. In this session, 31 papers were selected for publication, among which 20 papers are published in this special issue [1][2][3][4][5][6][7][8][9][10][11][12][13][14][15][16][17][18][19][20], two more [21,22] in the next issue, and 9 papers are published by Materials Research Innovations [23][24][25][26][27][28][29][30][31]. All papers underwent the standard peer-review process of the journal and were accepted for publication based on the evaluations of at least two independent anonymous reviewers.…”
mentioning
confidence: 99%