Yong-Ping Zhao
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Yong-Ping Zhao has a total of 76 co-authors. Here are the top co-authors by number of shared publications:
Huan Wu
9 shared publicationsHui-Jun Tan
Professor, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Qinhuai District, Nanjing 210016, China
7 shared publicationsYao-Bin Chen
Engineer, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China
7 shared publicationsBing Li
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China
6 shared publicationsHui-Jie Jin
Nanjing University of Aeronautics and Astronautics
4 shared publicationsYi Jin
4 shared publications
Latest Publications
- 22 September 2026
- Published by Elsevier in Measurement
- Vol. 292
Cross-modal schlieren-like image reconstruction of supersonic inlet flows from wall-pressure signals using a pressure-guided StyleGAN framework
- 22 September 2026
- Published by Elsevier in Measurement
- Vol. 292
Cross-modal schlieren-like image reconstruction of supersonic inlet flows from wall-pressure signals using a pressure-guided StyleGAN framework
- 10 June 2026
- Published by Elsevier in Measurement
- Vol. 284
An efficient multi-domain encoded fusion network for supersonic inlet condition detection
- 10 June 2026
- Published by Elsevier in Measurement
- Vol. 284
An efficient multi-domain encoded fusion network for supersonic inlet condition detection
- 30 May 2026
- Published by SAGE Publications in Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
A surge warning method for aero-engines based on multi-scale discrete wavelet transform fusion and lightweight convolutional neural network
Compressor surge in aero-engines is a primary cause of catastrophic engine failure, making precise early warning essential for flight safety. Prevailing methods commonly encounter a critical bottleneck when balancing accuracy with model efficiency, which restricts their practical engineering applications. To address this limitation, this paper proposes an aero-engine surge early warning method based on the Discrete Wavelet Transform (DWT) and a lightweight Convolutional Neural Network, termed Multiwave Fusion-based Lightweight Convolutional Neural Network (MF-LWCNN). The proposed method first employs DWT to decompose sensor signals into multiple scales, effectively separating and extracting high-frequency detail features and low-frequency trend features. Subsequently, transposed convolution is introduced to establish a scale-consistency learning mechanism. Combined with pointwise convolution, this mechanism achieves channel-wise feature fusion. This design circumvents the “manual dependency” issue inherent in traditional DWT feature selection. Meanwhile, a residual network is incorporated to enhance the model’s feature representation capability. Finally, a depthwise separable convolutional network is employed to construct the classification module for implementing surge early warning. To validate the efficacy, experiments were conducted on the public Case Western Reserve University bearing dataset and an experimental dataset from an aero-engine compressor test rig. The results demonstrate that MF-LWCNN offers significant advantages in both accuracy and lightweight model design, providing theoretical foundation and a technical reference for the engineering application of surge early warning technology.
- 30 May 2026
- Published by SAGE Publications in Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
A surge warning method for aero-engines based on multi-scale discrete wavelet transform fusion and lightweight convolutional neural network
Compressor surge in aero-engines is a primary cause of catastrophic engine failure, making precise early warning essential for flight safety. Prevailing methods commonly encounter a critical bottleneck when balancing accuracy with model efficiency, which restricts their practical engineering applications. To address this limitation, this paper proposes an aero-engine surge early warning method based on the Discrete Wavelet Transform (DWT) and a lightweight Convolutional Neural Network, termed Multiwave Fusion-based Lightweight Convolutional Neural Network (MF-LWCNN). The proposed method first employs DWT to decompose sensor signals into multiple scales, effectively separating and extracting high-frequency detail features and low-frequency trend features. Subsequently, transposed convolution is introduced to establish a scale-consistency learning mechanism. Combined with pointwise convolution, this mechanism achieves channel-wise feature fusion. This design circumvents the “manual dependency” issue inherent in traditional DWT feature selection. Meanwhile, a residual network is incorporated to enhance the model’s feature representation capability. Finally, a depthwise separable convolutional network is employed to construct the classification module for implementing surge early warning. To validate the efficacy, experiments were conducted on the public Case Western Reserve University bearing dataset and an experimental dataset from an aero-engine compressor test rig. The results demonstrate that MF-LWCNN offers significant advantages in both accuracy and lightweight model design, providing theoretical foundation and a technical reference for the engineering application of surge early warning technology.
- 17 May 2026
- Published by Elsevier in Measurement
- Vol. 280
A deep learning-based intelligent early warning system for aero-engine vibration anomalies
- 17 May 2026
- Published by Elsevier in Measurement
- Vol. 280
A deep learning-based intelligent early warning system for aero-engine vibration anomalies
- 23 September 2025
- Published by Elsevier in Expert Systems with Applications
- Vol. 298
Time-balanced MSE for machinery imbalanced degradation trend prediction
- 23 September 2025
- Published by Elsevier in Expert Systems with Applications
- Vol. 298
Time-balanced MSE for machinery imbalanced degradation trend prediction
- 8 February 2025
- Published by Elsevier in Expert Systems with Applications
- Vol. 272
Multi-level and multi-scale cross attention network of wavelet packet transform for supersonic inlet unstart prediction
- 8 February 2025
- Published by Elsevier in Expert Systems with Applications
- Vol. 272
Multi-level and multi-scale cross attention network of wavelet packet transform for supersonic inlet unstart prediction
- 17 December 2024
- Published by Elsevier in Aerospace Science and Technology
- Vol. 158
Multi-sensor flow state identification and schlieren image generation for supersonic inlet
- 17 December 2024
- Published by Elsevier in Aerospace Science and Technology
- Vol. 158
Multi-sensor flow state identification and schlieren image generation for supersonic inlet