Multi-fidelity Surrogate Model Based Wind Tunnel Structure Design Optimization-Reference-Cited by-同舟云学术

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Multi-fidelity Surrogate Model Based Wind Tunnel Structure Design Optimization

Published:2024-05-16 Issue: Volume:44 Page:72-78
ISSN:
Container-title:2024 16th International Conference on Advanced Computational Intelligence (ICACI)
language:
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Author:

Yisheng Yang¹,Zeyuan Yang¹,Xiqiang Yan²,Sijie Yan¹,Bowen Liu²,Han Ding¹

Affiliation:

1. Huazhong University of Science and Technology,State Key Lab of Digital Manufacturing Equipment and Technology,Wuhan,China

2. Facility Design and Instrument Institute,China Aerodynamics Research and Development Center,Mianyang,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10536986/10536996/10537024.pdf?arnumber=10537024

Reference32 articles.

1. Structure design and research of 5.5m×4m aeroacoustic wind tunnel;Yang;Acta Aeronauticaet Astronautica Sinica,2023

2. The general structural design for 2m supersonic wind tunnel;Yu;Journal of Experiments in Fluid Mechanics,2012

3. Optimized design of hypersonic wind tunnel test section;Sun;Mechanical Engineering & Automation,2012

4. Simulation technique of semi-flexible nozzle machine dynamic;Nie;Journal of Experiments in Fluid Mechanics,2012

5. Key technology for mechanical design in large-scale cryogenic wind tunnel;Lai;Journal of Experiments in Fluid Mechanics,2022

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