Please use this identifier to cite or link to this item:
http://irepo.futminna.edu.ng:8080/jspui/handle/123456789/29179
Title: | Structural Integrity Study for a Quadcopter Frame to Be Deployed for Pest Control |
Authors: | Ibrahim, Sulaiman Alkali, Babawuya Oyewole, Adedipe Bala Alhaji, Salihu Abdullahi, Aliyu Alhaji Ibrahim, Aku |
Keywords: | Bird control computational fluid dynamics structural analysis surveillance unmanned aerial vehicles |
Issue Date: | Sep-2021 |
Publisher: | EVERGREEN |
Abstract: | Quadcopters are one of the most versatile unmanned aerial vehicles deployed for various purposes. In this study it is going to be used as part of a system used for bird control therefore the structural integrity is investigated. The aim of the paper is to investigate the structural and aerodynamic behaviour of a quadcopter intended for bird control. A model of the drone has been developed in SolidWorks, then structural along with flow analysis carried out using ANSYS software. The structural analysis reveals a maximum stress of 39.13 MPa of the arm due to thrust and 2.6 MPa on the frame due to load which are within the safe range for use of purpose. |
URI: | http://irepo.futminna.edu.ng:8080/jspui/handle/123456789/29179 |
Appears in Collections: | Physics |
Files in This Item:
File | Description | Size | Format | |
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Paper Quadcoupter.pdf | 509.35 kB | Adobe PDF | View/Open |
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