Wing Design Optimization for a Long-Endurance UAV using FSI Analysis and the Kriging Method-Reference-Cited by-同舟云学术

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Wing Design Optimization for a Long-Endurance UAV using FSI Analysis and the Kriging Method

Published:2016-09-30 Issue:3 Volume:17 Page:423-431
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:International Journal of Aeronautical and Space Sciences

Author:

Son Seok-Ho,Choi Byung-Lyul,Jin Won-Jin,Lee Yung-Gyo,Kim Cheol-Wan,Choi Dong-Hoon

Publisher

The Korean Society for Aeronautical & Space Sciences

Cited by 6 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. Fluid Coupled Structural Analysis and Optimization of Expanded Polystyrene-Fiber-Reinforced Composite Wing of an Unmanned Aerial Vehicle;Mechanics of Composite Materials;2024-04-26

2. One-way fluid-material interaction study on a plunging UAV wing;Materials Today: Proceedings;2021-08

3. Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models;International Journal of Aviation, Aeronautics, and Aerospace;2021

4. Conceptual Design and Fluid Structure Interaction Analysis of a Solar Powered High-Altitude Pseudo-Satellite (HAPS) UAV Wing Model;Lecture Notes in Mechanical Engineering;2020-10-26

5. Rapidly Tuning the PID Controller Based on the Regional Surrogate Model Technique in the UAV Formation;Entropy;2020-05-06

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