Aerodynamic Analysis of Rotor Spacing and Attitude Transition in Tilt-Powered Coaxial Rotor UAV [PDF]
Complex aerodynamic characteristics and optimal control during the attitude transition of tilt-powered coaxial twin-rotor unmanned aerial vehicles (UAVs) represent key challenges in flight control design.
Wei Wu +4 more
doaj +6 more sources
Effect of tip spacing, thrust coefficient and turbine spacing in multi-rotor wind turbines and farms [PDF]
Large eddy simulations (LESs) are performed to study the wakes of a multi-rotor wind turbine configuration comprising four identical rotors mounted on a single tower.
N. S. Ghaisas +5 more
doaj +7 more sources
Aerodynamic performance of a Hex-rotor unmanned aerial vehicle with different rotor spacing
In this paper, an attempt was made to obtain the aerodynamic performance of a Hex-rotor unmanned aerial vehicle with different rotor spacing. The hover efficiency of the Hex-rotor unmanned aerial vehicle is analyzed by both experimental tests and ...
Yao Lei, Mingxin Cheng
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Effect of Rotor-Stator Spacing on Compressor Performance at Variable Operating Conditions
This paper investigates the effect of rotor-stator spacing and operating conditions on compressor performance and the rotor-stator interaction mechanism.
Han Niu, Jiang Chen, Hang Xiang
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Aerodynamic Characteristics of a Hex-Rotor MAV With Three Coaxial Rotors in Hover
In order to study the aerodynamic characteristics of a Hex-rotor micro aerial vehicle (MAV) with different rotor spacing, both experiments and numerical simulations are performed in this paper.
Yao Lei, Yiqiang Ye
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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
Yao Lei, Hengda Wang
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Experimental Investigation on Hover Performance of a Ducted Coaxial-Rotor UAV
This paper presents experimental investigations on aerodynamic performance of a ducted coaxial-rotor system to evaluate its potential application as a small unmanned aerial vehicle (SUAV).
Hai Li, Zaibin Chen, Hongguang Jia
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Effect of windage heating on a micro high-speed rotor-stator cavity
The main objective of this work is to investigate the effect of windage heating on the micro high-speed rotor-stator cavity. The influences of centrifugal force and spacing on the windage heating are analyzed with and without the change of gap ratio ...
Jianyu Liu +4 more
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Hover Performance Analyses of Coaxial Co-Rotating Rotors for eVTOL Aircraft
Hover performance analyses of coaxial co-rotating rotors (or stacked rotors), which can be used as lifting rotors for electric VTOL (eVTOL) aircraft, are conducted here.
Yu-Been Lee, Jae-Sang Park
doaj +1 more source
Aerodynamic Performance of V8 Octorotor MAV with Different Rotor Configurations in Hover
A new multirotor aerial vehicle with two rotor arms formed in a V-shape configuration is introduced in this paper. To figure out the aerodynamic interference effects between rotors as an implication of the control method, this paper discusses the ...
Yao Lei, Zhicheng Feng, Chensong Ma
doaj +1 more source

