Flutter Boundary Prediction Based on Feature Extraction and Bayesian Optimization Transformer–Long Short-Term Memory

A data-driven approach for flutter boundary prediction is proposed, which adopts a deep learning model to extract flutter features from measured signals, thereby enabling the analysis of aeroelastic system stability. Following a modeling strategy that leverages structural acceleration response signals, a dataset is constructed from experimental data acquired from wind tunnel tests, and a multidimensional feature system and a set of comparative models are subsequently established for performance evaluation. Comparative analytical results reveal that the integration of power spectral density (PSD) with the Bayesian optimization Transformer–long short-term memory hybrid model can markedly enhance the efficacy of feature extraction and the accuracy of flutter boundary prediction. Experimental validation demonstrates that the proposed method achieves a mean prediction error of 3.73% for unseen working conditions of the wind tunnel model and 4.14% for data obtained from a single flight test sortie. Furthermore, a prediction error below 10% is achievable at approximately 70% of the critical flutter speed, which could contribute to enhanced early warning performance in flutter tests.

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Publication Details

Journal
Journal of Aircraft
Published
2026-06-13
DOI
https://doi.org/10.2514/1.c038983
Primary Topic
Aeroelasticity and Vibration Control
Type
article
Field-Weighted Citation Impact
0.00
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article

Flutter Boundary Prediction Based on Feature Extraction and Bayesian Optimization Transformer–Long Short-Term Memory

Yue Wang, Li Zhou
Journal of Aircraft
Aeroelasticity and Vibration Control
article

Flutter Boundary Prediction Based on Feature Extraction and Bayesian Optimization Transformer–Long Short-Term Memory

Yue Wang, Li Zhou
article en

Abstract

A data-driven approach for flutter boundary prediction is proposed, which adopts a deep learning model to extract flutter features from measured signals, thereby enabling the analysis of aeroelastic system stability. Following a modeling strategy that leverages structural acceleration response signals, a dataset is constructed from experimental data acquired from wind tunnel tests, and a multidimensional feature system and a set of comparative models are subsequently established for performance evaluation. Comparative analytical results reveal that the integration of power spectral density (PSD) with the Bayesian optimization Transformer–long short-term memory hybrid model can markedly enhance the efficacy of feature extraction and the accuracy of flutter boundary prediction. Experimental validation demonstrates that the proposed method achieves a mean prediction error of 3.73% for unseen working conditions of the wind tunnel model and 4.14% for data obtained from a single flight test sortie. Furthermore, a prediction error below 10% is achievable at approximately 70% of the critical flutter speed, which could contribute to enhanced early warning performance in flutter tests.

Journal of Aircraft
Nanjing University of Aeronautics and Astronautics (CN)
Affordable and clean energy
Openalex Percentile: Top 2%
Aeroelasticity and Vibration Control
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Flutter Boundary Prediction Based on Feature Extraction and Bayesian Optimization Transformer–Long Short-Term Memory — Yue Wang, Li Zhou · Journal of Aircraft (2026) | TGRS Research Map | TGRS