Aerodynamic structural design and control for a new miniature coaxial dual-rotor unmanned aerial vehicle

B Yan, P Cheng, C Cai - … , Part I: Journal of Systems and …, 2023 - journals.sagepub.com
This article mainly introduces a design and control method for a new type of portable coaxial
dual-rotor unmanned aerial vehicle. The coaxial dual-rotor unmanned aerial vehicle …

螺旋桨安装效应对无人机气动特性影响

史文博, 李杰 - 航空动力学报, 2020 - jasp.com.cn
为解决某型飞翼布局无人机(UAV) 带动力构型风洞试验最大升阻比相对无动力状态大幅下降的
问题, 采用计算流体动力学(CFD) 方法对无人机无动力与带动力构型进行了数值模拟 …

Investigation and Improvement of Pusher-Propeller Installation Effect for Flying Wing UAV

W Shi, J Li, S Zhao, Z Yang - … Journal of Aeronautical and Space Sciences, 2021 - Springer
This paper presents a collaborative experimental and numerical research to investigate the
influences of the installation of propeller on aircraft aerodynamic performance, and two …

A configuration-independent modeling toolset for the analysis of small-scale electric-powered UAVs

RH Gautier, ZC Fisher, CB McMillan… - 2018 AIAA Modeling …, 2018 - arc.aiaa.org
Small-scale electric-powered unmanned aerial vehicles (UAVs) are increasingly used in a
variety of commercial, civil and military applications. They take on many forms, among which …