Prediction of Aerodynamic Forces at the Tip of the Compressor Blades Based on Multi-scale 1DCNN Combined with CBAM-Reference-Cited by-同舟云学术

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Prediction of Aerodynamic Forces at the Tip of the Compressor Blades Based on Multi-scale 1DCNN Combined with CBAM

Published:2024-10 Issue: Volume:203 Page:112190
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Yao Minghui,Wu Shaohua^ORCID,Niu Yan,Wu Qiliang^ORCID,Song Renduo,Bai Bin

Funder

Tianjin Municipal Natural Science Foundation

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference37 articles.

1. Aerodynamic analysis and design optimization of a centrifugal compressor impeller considering realistic manufacturing uncertainties;Ju;Aerosp. Sci. Technol.,2021

2. Aircraft engines and gas turbines;Kerrebrock,1992

3. Nonlinear resonance and chaotic dynamic of rotating graphene platelets reinforced metal foams plates in thermal environment;Song;Arch. Civ. Mech. Eng.,2024

4. Review of design optimization methods for turbomachinery aerodynamics;Li;Prog. Aerosp. Sci.,2017

5. Effect of double crack on fatigue crack growth life of 3D printing compressor impeller;Qu;Thin-Walled Struct,2023

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

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

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