Structural Integrity Study for a Quadcopter Frame to Be Deployed for Pest Control

Please use this identifier to cite or link to this item: http://irepo.futminna.edu.ng:8080/jspui/handle/123456789/29179

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DC Field	Value	Language
dc.contributor.author	Ibrahim, Sulaiman	-
dc.contributor.author	Alkali, Babawuya	-
dc.contributor.author	Oyewole, Adedipe	-
dc.contributor.author	Bala Alhaji, Salihu	-
dc.contributor.author	Abdullahi, Aliyu Alhaji	-
dc.contributor.author	Ibrahim, Aku	-
dc.date.accessioned	2025-05-05T15:16:44Z	-
dc.date.available	2025-05-05T15:16:44Z	-
dc.date.issued	2021-09	-
dc.identifier.uri	http://irepo.futminna.edu.ng:8080/jspui/handle/123456789/29179	-
dc.description.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.	en_US
dc.language.iso	en_US	en_US
dc.publisher	EVERGREEN	en_US
dc.subject	Bird control	en_US
dc.subject	computational fluid dynamics	en_US
dc.subject	structural analysis	en_US
dc.subject	surveillance	en_US
dc.subject	unmanned aerial vehicles	en_US
dc.title	Structural Integrity Study for a Quadcopter Frame to Be Deployed for Pest Control	en_US
dc.type	Article	en_US
Appears in Collections:	Physics

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