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://repository.futminna.edu.ng:8080/jspui/handle/123456789/18110

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DC Field	Value	Language
dc.contributor.author	Abdullahi, Aliyu Alhaji	-
dc.contributor.author	Sulaiman, Ibrahim	-
dc.contributor.author	Ibrahim, Ibrahim Aku G.	-
dc.date.accessioned	2023-02-15T11:44:25Z	-
dc.date.available	2023-02-15T11:44:25Z	-
dc.date.issued	2021-09-01	-
dc.identifier.uri	http://repository.futminna.edu.ng:8080/jspui/handle/123456789/18110	-
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	en_US
dc.publisher	EVERGREEN Joint Journal of Novel Carbon Resource Sciences & Green Asia Strategy	en_US
dc.subject	Bird control	en_US
dc.subject	computational fluid dynamics	en_US
dc.title	Structural Integrity Study for a Quadcopter Frame to be Deployed for Pest Control	en_US
Appears in Collections:	Mechanical Engineering

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