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Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (7): 228952-228952.doi: 10.7527/S1000-6893.2023.28952

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles     Next Articles

Fatigue life prediction of 2014-T6 aluminum alloy based on CDM theory and SVM model

Tongzhou GAO1, Xiaofan HE1, Xiaolei WANG2, Ziguang LI2, Zhentao ZHU2, Zhixin ZHAN1()   

  1. 1.School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China.
    2.Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China
  • Received:2023-05-03 Revised:2023-05-22 Accepted:2023-06-07 Online:2024-04-15 Published:2023-06-09
  • Contact: Zhixin ZHAN E-mail:zzxupc@163.com
  • Supported by:
    National Natural Science Foundation of China(12002011)

Abstract:

Based on the Continuous Damage Mechanics (CDM) theory and Support Vector Machine (SVM) model, a novel fatigue life prediction method has been developed to improve the accuracy of fatigue life prediction for 2014-T6 aluminum alloy materials. Firstly, by adopting the continuous damage mechanics model and the secondary development of the Abaqus-based UMAT subroutine, a damage mechanics finite element numerical implementation method for predicting the fatigue life of 2014-T6 aluminum alloy is established, and a calibration method for material parameters based on the particle swarm optimization algorithm is proposed. Subsequently, to further optimize the prediction results, the SVM model is employed to train the errors of fatigue life prediction results based on damage mechanics, thereby correcting the numerical prediction results. By comparing the prediction results of damage mechanics finite element, the SVM model-corrected prediction results, and experimental results, it is found that the accuracy of the SVM model-corrected prediction results is higher, verifying the applicability of the proposed method. This provides an effective solution for the fatigue life prediction of 2014-T6 aluminum alloy and is expected to play a significant role in practical engineering applications.

Key words: damage mechanics, support vector machine, aluminum alloy, fatigue, life prediction

CLC Number: