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Please use this identifier to cite or link to this item: http://ir.futminna.edu.ng:8080/jspui/handle/123456789/9318
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dc.contributor.authorIbrahim, Sulaiman-
dc.contributor.authorAlkali, Babawuya-
dc.contributor.authorOyewole, Adedipe-
dc.contributor.authorSalihu, Bala A.-
dc.contributor.authorAbdullahi, Aliyu Alhaji-
dc.contributor.authorG, Ibrahim Aku-
dc.date.accessioned2021-07-14T11:12:38Z-
dc.date.available2021-07-14T11:12:38Z-
dc.date.issued2020-12-
dc.identifier.citationS. Ibrahim, B. Alkali, A. Oyewole, S. B. Alhaji, A. A. Abdullahi, and I. A. G, “Preliminary structural integrity investigation for quadcopter frame to be deployed for pest control,” no. December, pp. 176–177, 2020.en_US
dc.identifier.urihttp://repository.futminna.edu.ng:8080/jspui/handle/123456789/9318-
dc.description.abstractQuadcopters 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 shows promising results as the stress built up due to the loads applied are within the safe range.en_US
dc.language.isoenen_US
dc.subjectQuadcoptersen_US
dc.subjectstructureen_US
dc.subjectanalysisen_US
dc.titlePreliminary structural integrity investigation for quadcopter frame to be deployed for pest controlen_US
dc.typeArticleen_US
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