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

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