Skip to content
DraconiticResearch
Search Sources API
197,761 studies31 sourcesUpdated 30 min ago
PreprintCC BY 4.0arXiv

A panoramic aerodynamic performance prediction method for turbomachinery cascades using transformer-enhanced neural operator

Abstract

To enable flexible and rapid aerodynamic performance evaluation in turbomachinery design, this paper proposes a panoramic performance prediction framework. Unlike most previous prediction models that directly predict the objective functions of interest, our approach first predicts the basic parameters of the Navier-Stokes equations, such as temperature, pressure, and density. Utilizing these basic physical quantities, it subsequently predicts key performance parameters of the turbine stage meridian plane. By adopting this methodology, our proposed panoramic performance prediction framework functions similarly to a CFD simulator, capable of predicting various objective of interest to the designers. To enhance prediction accuracy, a transformer-enhanced neural operator (TNO) is introduced within this framework. Using the Rotor 37 blades as a reference, the proposed TNO is trained to predict the performance of a transonic compressor blade in the meridian plane. The TNO can accurately predict total quantities such as isentropic efficiency, mass flow, and distributions of total pressure ratio. Remarkably, the prediction error of TNO is observed to be smaller than that of state-of-the-art deep learning operators such as the FNO and DeepONet. Furthermore, the TNO is applied to downstream tasks, including sensitivity analysis and optimization of various objective functions. The results confirm that the TNO can operate almost like a CFD simulator, while reducing the computational cost of downstream tasks by four orders of magnitude. The effectiveness and reliability of the proposed TNO for solving different kinds of downstream tasks have been well demonstrated.

Versions

Related

  1. CoPiT: A conditional Position-induced Transformer for aerodynamic field prediction on unstructured meshes
    Junfeng Chen, Yongchen Fan, Zhonghua Qiao +1
    arXivPreprintCC BY-NC-ND 4.0Full textNumerical analysis & scientific computingComputational physicsarXiv
  2. Three-dimensional effects on the aerodynamic performance of flapping wings in tandem configuration
    G. Arranz, Oscar Flores, M. García-Villalba
    Journal of Fluids and StructuresPeer-reviewedLicence not statedFull text51 citedFluid dynamicsHAL
  3. Effect of leading edge geometry on aerodynamic performance of a flat plate
    Intesaaf Ashraf, Hamid Hassan Khan, Majid Hassan Khan
    arXivPreprintarXiv licenceFull textFluid dynamicsarXiv
  4. Neural Field Ensembles for Aerodynamic Surface Prediction: Winning Solution to the ONERA CRM Wall Distribution 2025 Challenge
    Lionel Salesses, Caroline Sainvitu, Tariq Benamara
    arXivPreprintCC BY 4.0Full textFluid dynamicsarXiv
  5. HGPTrans: Hierarchical Graph-Pooling Transolver for Automotive Aerodynamic Drag Coefficient Prediction
    Bo Liu, Fengli Zhang, Qiuli Luo +2
    arXivPreprintarXiv licenceFull textFluid dynamicsarXiv
BibTeX
@misc{wang2026panoramic,
  title = {{A panoramic aerodynamic performance prediction method for turbomachinery cascades using transformer-enhanced neural operator}},
  author = {Qineng Wang and Zhendong Guo and Liming Song and Tianyuan Liu},
  howpublished = {arXiv},
  year = {2026},
  month = sep,
  doi = {10.48550/arxiv.2609.16066},
  eprint = {2609.16066},
  archivePrefix = {arXiv},
  url = {https://arxiv.org/abs/2609.16066},
  note = {CC BY 4.0},
}
RIS
TY  - UNPB
TI  - A panoramic aerodynamic performance prediction method for turbomachinery cascades using transformer-enhanced neural operator
AU  - Qineng Wang
AU  - Zhendong Guo
AU  - Liming Song
AU  - Tianyuan Liu
PY  - 2026
DA  - 2026/09/13
PB  - arXiv
DO  - 10.48550/arxiv.2609.16066
UR  - https://arxiv.org/abs/2609.16066
AB  - To enable flexible and rapid aerodynamic performance evaluation in turbomachinery design, this paper proposes a panoramic performance prediction framework. Unlike most previous prediction models that directly predict the objective functions of interest, our approach first predicts the basic parameters of the Navier-Stokes equations, such as temperature, pressure, and density. Utilizing these basic physical quantities, it subsequently predicts key performance parameters of the turbine stage meridian plane. By adopting this methodology, our proposed panoramic performance prediction framework functions similarly to a CFD simulator, capable of predicting various objective of interest to the designers. To enhance prediction accuracy, a transformer-enhanced neural operator (TNO) is introduced within this framework. Using the Rotor 37 blades as a reference, the proposed TNO is trained to predict the performance of a transonic compressor blade in the meridian plane. The TNO can accurately predict total quantities such as isentropic efficiency, mass flow, and distributions of total pressure ratio. Remarkably, the prediction error of TNO is observed to be smaller than that of state-of-the-art deep learning operators such as the FNO and DeepONet. Furthermore, the TNO is applied to downstream tasks, including sensitivity analysis and optimization of various objective functions. The results confirm that the TNO can operate almost like a CFD simulator, while reducing the computational cost of downstream tasks by four orders of magnitude. The effectiveness and reliability of the proposed TNO for solving different kinds of downstream tasks have been well demonstrated.
ER  -