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Research paper | Publishing Language: Chinese | Open Access

Research on fatigue failure mechanism and life prediction method of FGH96 flat plate with a hole

Chengli DONG1,2,3Jiangbo FAN4Qiyu LU4Duoqi SHI4Guangping GUO1,2,3( )
AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
AECC Key Laboratory of Material Testing and Evaluation,Beijing 100095,China
Beijing Key Laboratory of Aeronautical Material Testing and Evaluation,Beijing 100095,China
School of Energy and Power Engineering,Beihang University,Beijing 100191,China
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Abstract

Fatigue tests were conducted on FGH96 flat plates containing a hole at 600 ℃. Utilizing a viscoplastic constitutive model, the stress and plastic strain distributions within these plates were meticulously calculated. Scanning electron microscopy(SEM) was employed to analyze the fatigue failure mechanism. Based on SEM observations and the geometric attributes of the FGH96 plates with holes, the critical fatigue damage and stress concentration coefficient were defined. Subsequently, the CDM(cumulative damage model)was refined accordingly. The findings revealed that, in comparison to conventional fatigue life prediction techniques, the revised CDM model, which incorporates critical fatigue damage and stress concentration coefficients, exhibited enhanced prediction accuracy for the fatigue life of FGH96 flat plates with holes. Notably, all prediction results fell within a ±2 error band.

CLC number: V231.95 Document code: A

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Journal of Aeronautical Materials
Pages 102-109

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Cite this article:
DONG C, FAN J, LU Q, et al. Research on fatigue failure mechanism and life prediction method of FGH96 flat plate with a hole. Journal of Aeronautical Materials, 2025, 45(2): 102-109. https://doi.org/10.11868/j.issn.1005-5053.2024.000082

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Received: 15 May 2024
Published: 01 April 2025
© Journal of Aeronautical Materials 2025.

This is an open access article under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).