An experimental procedure to estimate damage evolution and remaining fatigue life of metals associated with fatigue loading is presented. Experimental phase involves uniaxial tension-compression fatigue tests performed with solid API 5L X52 and tubular carbon steel 1018 specimens subjected to both constant and variable amplitude loading. A correlation between the so-called damage parameter and the thermal response of a material at different damage levels is proposed. Results demonstrate that the correlation can estimate damage evolution with reasonable accuracy in both constant and variable amplitude fatigue processes. It is shown that under the conditions tested the evolution of damage parameter with respect to the normalized fatigue life is independent of the load amplitude, load ratio, loading sequence, material properties, and specimen geometry. The proposed correlation and the relationship between the damage parameter and the normalized fatigue life are employed to develop a non-destructive method to predict the remaining fatigue life of metallic specimens with prior fatigue damage. The method is applied to both constant and variable amplitude loading and the predicted results are found to be in good agreement with those obtained from the experiments. (C) 2013 Elsevier Ltd. All rights reserved.
机构:
Institute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang UniversityInstitute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang University
Zhixin ZHAN
Weiping HU
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Institute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang UniversityInstitute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang University
Weiping HU
Miao ZHANG
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China Academy of Space TechnologyInstitute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang University
Miao ZHANG
Qingchun MENG
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Institute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang UniversityInstitute of Solid Mechanics, School of Aeronautics Science and Engineering,BeiHang University
机构:
Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Chen, Zhanguang
Zheng, Tao
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Zheng, Tao
Sun, Rongqing
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China Aerosp Res Inst Mat & Proc Technol, Beijing 100076, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Sun, Rongqing
Zhang, Li
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Zhang, Li
Wang, Zhongyu
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Wang, Zhongyu
Zhou, Jindi
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Zhou, Jindi
Han, Xiaojian
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Han, Xiaojian
Yu, Shangyang
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
Yu, Shangyang
Guo, Licheng
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Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China