UAV Wing Design via Efficient Global Optimization-Reference-Cited by-同舟云学术

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UAV Wing Design via Efficient Global Optimization

Published:2024-02-28 Issue: Volume:37 Page:62-66
ISSN:
Container-title:2024 16th International Conference on Knowledge and Smart Technology (KST)
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Author:

Risanthia Anonphong¹,Phiboon Tharathep²,Bureerat Sujin³,Pichitkul Auraluck¹,Tantrairatn Suradet¹,Ariyarit Atthaphon¹

Affiliation:

1. School of Mechanical Engineering, Institute of Engineering, Suranaree University of Technology,Nakhon Ratchasima,Thailand

2. Institute of Research and Development, Suranaree University of Technology,Nakhon Ratchasima,Thailand

3. Khon Kaen University,Faculty of Engineering,Department of Mechanical Engineering,Khon Kaen,Thailand

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10499640/10499641/10499662.pdf?arnumber=10499662

Reference14 articles.

1. Planform dependency of optimum cross-sectional geometric distributions for supersonic wing

2. Application of Low- and High-Fidelity Simulation Tools to Helicopter Rotor Blade Optimization

3. A two-stage adaptive multi-fidelity surrogate model-assisted multi-objective genetic algorithm for computationally expensive problems;Qi;Engineering with computers,2021

4. Design, performance evaluation and optimization of a UAV

5. An efficient aerodynamic shape optimization of blended wing body UAV using multi-fidelity models

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