Aerodynamic Performance of an Octorotor SUAV with Different Rotor Spacing in Hover

Aerodynamic Performance of an Octorotor SUAV with Different Rotor Spacing in Hover

To study the aerodynamic performance of hovering octorotor small unmanned aerial vehicles (SUAV) with different rotor spacing, the computational fluid dynamics (CFD) method is applied to analyze the flow field of an octorotor SUAV in detail. In addition, an experimental platform is built to measure...

Full description

Bibliographic Details
Main Authors: Yao Lei, Yuhui Huang, Hengda Wang
Format: Article
Language:English
Published: MDPI AG 2020-10-01
Series:Processes
Subjects:
octorotor SUAV
aerodynamic performance
rotor spacing
hover
CFD
vortices distribution
Online Access:https://www.mdpi.com/2227-9717/8/11/1364

Internet

https://www.mdpi.com/2227-9717/8/11/1364

Similar Items