CFD-based Thrust Analysis of Unmanned Aerial Vehicle in Hover Mode: Effects of Single Rotor Blade Shape-Reference-Cited by-同舟云学术

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CFD-based Thrust Analysis of Unmanned Aerial Vehicle in Hover Mode: Effects of Single Rotor Blade Shape

Published:2014-05-01 Issue:5 Volume:38 Page:513-520
ISSN:1226-4873
Container-title:Transactions of the Korean Society of Mechanical Engineers A
language:en
Short-container-title:Transactions of the Korean Society of Mechanical Engineers A

Author:

Yun Jae Hyun,Choi Ha-Young,Lee Jongsoo

Publisher

The Korean Society of Mechanical Engineers

Subject

Mechanical Engineering

Cited by 8 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 Performance Evaluation of a Coaxial Octocopter Based on Taguchi Method;Journal of Fluids Engineering;2024-04-15

2. Multi-objective Optimization of Aerodynamic Blade Shapes for Quadcopter System to Enhance Hovering Thrust and Power Consumption Efficiency;International Journal of Aeronautical and Space Sciences;2023-05-06

3. Design and modal analysis of a Quadcopter propeller through finite element analysis;Materials Today: Proceedings;2021

4. Modeling and Mechanical Vibration characteristics analysis of a Quadcopter Propeller using FEA;IOP Conference Series: Materials Science and Engineering;2019-11-01

5. Design of a Thrust Tester to Verify the Thrust Performance of a Blade of an Unmanned Aerial Vehicle;Transactions of the Korean Society of Mechanical Engineers - A;2018-06-30

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