A tensor basis neural network-based turbulence model for transonic axial compressor flows-Reference-Cited by-同舟云学术

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A tensor basis neural network-based turbulence model for transonic axial compressor flows

Published:2024-06 Issue: Volume:149 Page:109155
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ji Ziqi^ORCID,Du Gang^ORCID

Publisher

Elsevier BV

Reference54 articles.

1. Lessons from rotor 37;Denton;J. Therm. Sci.,1997

2. Uncertainty quantification of Spalart–Allmaras turbulence model coefficients for simplified compressor flow features;He;J. Fluids Eng.,2020

3. Three-dimensional flowfields inside a transonic compressor with swept blades;Hah,1990

4. Assessment of three turbulence models in a compressor rotor;Shabbir,1996

5. Swift code assessment for two similar transonic compressors;Chima,2009

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1. Aerodynamic force prediction of compressor blade surfaces based on machine learning;Physics of Fluids;2024-08-01

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