4.5 Article

Real-Time Prediction of Probabilistic Crack Growth with a Helicopter Component Digital Twin

期刊

AIAA JOURNAL
卷 -, 期 -, 页码 -

出版社

AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J060890

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资金

  1. National Natural Science Foundation of China [12072011]
  2. Aeronautical Science Foundation of China [201909051001]
  3. Seed Foundation of Beijing Advanced Discipline Center for Unmanned Aircraft System [ADBUAS-2019-SP-05]

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In this paper, a reduced-order simulation approach is developed to achieve real-time prediction of crack growth in complex structures. By combining symmetric Galerkin boundary element method-finite element method (SGBEM-FEM) coupling method with machine learning methods, the proposed approach can automatically simulate hundreds of crack samples and establish the relation between crack sizes/shapes and crack-front stress intensity factors. This method provides a key simulation technology for realizing the digital twin of complex structures.
To deploy the airframe digital twin or to conduct probabilistic evaluations of the remaining life of a structural component, a (near) real-time crack-growth simulation method is critical. In this paper, a reduced-order simulation approach is developed to achieve this goal by leveraging two methods. On the one hand, the symmetric Galerkin boundary element method-finite element method (SGBEM-FEM) coupling method is combined with parametric modeling to generate the database of computed stress intensity factors for cracks with various sizes/shapes in a complex structural component, by which hundreds of samples are automatically simulated within a day. On the other hand, machine learning methods are applied to establish the relation between crack sizes/shapes and crack-front stress intensity factors. By combining the reduced-order computational model with load inputs and fatigue growth laws, a real-time prediction of probabilistic crack growth in complex structures with minimum computational burden is realized. In an example of a round-robin helicopter component, even though the fatigue crack growth is simulated cycle by cycle, the simulation is faster than real-time (as compared with the physical test). The proposed approach is a key simulation technology toward realizing the digital twin of complex structures, which further requires fusion of model predictions with flight/inspection/monitoring data.

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