Feed-Forward Neural Network-Based Prediction of Flutter Speed of 3 DOF 2D Wing Model

Abstract Introduction The application of artificial intelligence, particularly neural network models, has expanded throughout various fields of academic and industrial studies, recently. This research focuses to investigate aeroelastic phenomena and predict flutter speeds without expensive computational and experimental methods utilizing these algorithms, specifically the artificial neural network (ANN). Methods Fundamentally, the approach involves an ANN algorithm to navigate the complexities of aeroelastic systems, achieved by layering multiple ANNs. The network's neurons effectively interpret diverse flight data by this structure. The study also incorporates state-space representation and Theodorsen's unsteady aerodynamic theory to create a comprehensive dataset on aeroelastic flutter speed across different wing parameters. In order to forecast the flutter speeds, a feed-forward neural network (FFNN) model, which is an approach of ANN method, containing sigmoid hidden neurons and a linear output neuron has been proposed for the conditions above. Results The proposed model accomplished a regression value of 0.92 for flutter speeds according to the experimental findings. As presented, the suggested FFNN model is successful and can be employed to predict the flutter speed estimation. The findings of the FFNN structure are validated with the previous work for aeroelastic flutter speed analysis in the literature. Discussion Finally, the findings indicate that the FFNN model formulated in this study is highly accurate in predicting flutter speeds with the accordance of numerical results of aeroelastic structure modeled with unsteady aerodynamic theory. In addition, the correctness of the predicted flutter speeds demonstrates that analyzing without expensive tests and high computational costs is in the near future.

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Publication Details

Journal
Journal of Vibration Engineering & Technologies
Published
2025-01-01
DOI
https://doi.org/10.1007/s42417-024-01741-1
Citations
2
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
9.99

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article

Feed-Forward Neural Network-Based Prediction of Flutter Speed of 3 DOF 2D Wing Model

Metin O. Kaya, Can Eyüpoğlu, Osman Dağlı
2 citations
Journal of Vibration Engineering & Technologies
Aerospace and Aviation Technology
9.99
article

Feed-Forward Neural Network-Based Prediction of Flutter Speed of 3 DOF 2D Wing Model

Metin O. Kaya, Can Eyüpoğlu, Osman Dağlı
article en
2 citations

Abstract

Abstract Introduction The application of artificial intelligence, particularly neural network models, has expanded throughout various fields of academic and industrial studies, recently. This research focuses to investigate aeroelastic phenomena and predict flutter speeds without expensive computational and experimental methods utilizing these algorithms, specifically the artificial neural network (ANN). Methods Fundamentally, the approach involves an ANN algorithm to navigate the complexities of aeroelastic systems, achieved by layering multiple ANNs. The network's neurons effectively interpret diverse flight data by this structure. The study also incorporates state-space representation and Theodorsen's unsteady aerodynamic theory to create a comprehensive dataset on aeroelastic flutter speed across different wing parameters. In order to forecast the flutter speeds, a feed-forward neural network (FFNN) model, which is an approach of ANN method, containing sigmoid hidden neurons and a linear output neuron has been proposed for the conditions above. Results The proposed model accomplished a regression value of 0.92 for flutter speeds according to the experimental findings. As presented, the suggested FFNN model is successful and can be employed to predict the flutter speed estimation. The findings of the FFNN structure are validated with the previous work for aeroelastic flutter speed analysis in the literature. Discussion Finally, the findings indicate that the FFNN model formulated in this study is highly accurate in predicting flutter speeds with the accordance of numerical results of aeroelastic structure modeled with unsteady aerodynamic theory. In addition, the correctness of the predicted flutter speeds demonstrates that analyzing without expensive tests and high computational costs is in the near future.

Journal of Vibration Engineering & TechnologiesVol. 13(1)
Istanbul Technical University (TR), Turkish Air Force Academy (TR)
Türkiye Bilimsel ve Teknolojik Araştırma Kurumu, Istanbul Teknik Üniversitesi, Bilimsel Araştırma Projeleri Birimi, İstanbul Teknik Üniversitesi
Openalex Percentile: Top 4%
Aerospace and Aviation Technology
9.99
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