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- W3204315044 abstract "The strain information and loads conditions of composite wings are important basis for aircraft health evaluation. In this paper, firstly to demonstrate the accuracy of Fiber Bragg Grating (FBG) sensors and provide guidance for the following study, experiment is carried out to study the effect of the adhesive layer thickness on the strain transfer. Then finite element analysis software ABAQUS is applied to analyze the strain distribution, and the simulation data is used to fit the pseudo-Kriging interpolation model to invert the strain information of crucial points. Finally, K-BP model is proposed by combining the interpolation model with back propagation (BP) neural network, which can be used to improve the accuracy on both strain field inversion and load identification. The results show that the proposed model can achieve great load identification results with fewer samples and optimize the interpolation parameters at the same time, which could provide important basis for evaluating the accuracy of strain field." @default.
- W3204315044 created "2021-10-11" @default.
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- W3204315044 date "2022-01-01" @default.
- W3204315044 modified "2023-10-11" @default.
- W3204315044 title "K-BP neural network-based strain field inversion and load identification for CFRP" @default.
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- W3204315044 doi "https://doi.org/10.1016/j.measurement.2021.110227" @default.
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