A Continuum Damage Mechanics Approach for Fatigue Life Prediction of Open-Hole Metallic Plate

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A damage evolution model is presented for fatigue life prediction of metallic structures. This model is formulated based on damage mechanics and the irreversible thermodynamics framework developed by LEMAITRE and CHABOCHE. Using this model, the fatigue lifetime can be predicted both in the high cycle fatigue (HCF) regime and the low cycle fatigue (LCF) regime. Based on the energy theory and material fatigue test data, the plastic strain threshold for damage initiation was modified for HCF and LCF respectively. The damage evolution parameters were determined according to the fatigue test results of standard specimens. A damage mechanics-finite element full-couple method was adopted to simulate the process of fatigue damage evolution. The numerical simulation of fatigue lives were compared with the fatigue tests of 2A12-T4 open-hole plates and good agreement was obtained.

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1060-1067

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October 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Wei Huang, Qin Sun: Mechanical Science and Technology for Aerospace Engineering, 2008, 27( 6) : 774 -778(In Chinese).

Google Scholar

[2] MOHANTY J R, VERMA B B, RAY P K: International Journal of Fatigue, 2009, 31(3): 418−424.

Google Scholar

[3] MOHANTY J R, VERMA B B, RAY P K: International Journal of Fatigue, 2009, 31(3): 425−432.

Google Scholar

[4] LEMAITRE J: Nuclear Engineering and Design, 1984, 80(2): 233−245.

Google Scholar

[5] XIAO Y C, LI S, GAO Z: International Journal of Fatigue, 1998, 20(7): 503−508.

Google Scholar

[6] DESMORAT R, KANE A, SEYEDI M: European Journal of Mechanics: A/Solids, 2007, 26(6): 909-935.

Google Scholar

[7] Chaboche JL, Lesne PM: Fatigue and Fracture of Engineering Materials and Structures, 1988, 11(1): 1-7.

Google Scholar

[8] Kim TW, Kang DH, Yeom JT, etc: Scripta Materialia, 2007, 57: 1149-1152.

Google Scholar

[9] Krajcinovic D, Lemaitre J: Continum damage mechanics theory and applications (Wien: Springer-Verlag, 1987).

Google Scholar

[10] Lemaitre J: A course on damage mechanics (Springer, 1996).

Google Scholar

[11] Lemaitre J, Desmorat R: Engineering damage mechanics (Berlin: Springer, 2005).

Google Scholar

[12] Dattoma V, Giancane S, Nobile R, etc: Int.J. Fatigue, 2006, 28: 85-95.

Google Scholar

[13] Desmorat R, Gatuingt F, Ragueneau F: Engineering Fracture Mechanics, 2007, 74(10): 1539-1560.

DOI: 10.1016/j.engfracmech.2006.09.012

Google Scholar

[14] Desmorat R, Kane A, Seyedi M, etc: European Journal of Mechanics-A/ Solids, 2007, 26(6): 909-935.

Google Scholar

[15] Desmorat B, Desmorat R: Comptes Rendus Mecanique, 2008, 336(5): 448-453.

DOI: 10.1016/j.crme.2008.01.001

Google Scholar

[16] Kachanov LM: Izv A Rad Nauk SSSR otd Tekh Nauk, 1958(8): 23-31.

Google Scholar

[17] Lemaitre J, Desmorat R: Engineering damage mechanics (Berlin: Springer, 2005).

Google Scholar

[18] Fengping Yang , Qin Sun, Jinheng Luo, Hua Zhang: Chinese Journal of Theoretical and Applied Mechanics, 2012, 44(001): 140-147.

Google Scholar

[19] Weixing Yao: Fatigue Life Prediction of Structures (Peking:National Defence Industry Press, 2004( In Chinese).

Google Scholar

[20] Minggao Yan, Bocao Liu, Jingui Li et al: China Aeronautical Materials Handbook, Part Ⅲ (Peking:China Standard Press, 2002. 39-83(In Chinese).

Google Scholar

[21] Yuya Wang, Enhou Han, Qunzhi Chen: Journal of Mechanical Strength, 2004, 26(S): 163-164(In Chinese).

Google Scholar

[22] Liu Jianxiu, Ding Suiliang: Journal of Mechanical Strength. 1999, 21(2): 157-158(In Chinese).

Google Scholar

[23] Gao Zhentong, Liu Zhijing, Jia Guorong, Handbook of fatigue properties of Aeronautical Materials (Peking:Beijing Institute of Aeronautical Materials, 1981(In Chinese).

Google Scholar