Aerodynamic Optimization of a Micro Quadrotor Aircraft with Different Rotor Spacings in Hover

In order to study the aerodynamic performance of the quadrotor with different rotor spacings in hover, experiments were performed together with numerical simulations. For experimental study, an experimental platform was designed to measure the thrust and power consumption of the quadrotor with diffe...

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Bibliographic Details
Main Authors: Yao Lei, Hengda Wang
Format: Article
Language:English
Published: MDPI AG 2020-02-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/10/4/1272