Please use this identifier to cite or link to this item:
http://repository.futminna.edu.ng:8080/jspui/handle/123456789/26931Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Sulaiman, Ibrahim | - |
| dc.contributor.author | Babawuya, Alkali | - |
| dc.contributor.author | Adedipe, Oyewole | - |
| dc.contributor.author | Salihu, Bala Alhaji | - |
| dc.contributor.author | Aliyu, Alhaji Abdullahi | - |
| dc.contributor.author | Ibrahim, Aku G. | - |
| dc.date.accessioned | 2024-03-09T08:22:35Z | - |
| dc.date.available | 2024-03-09T08:22:35Z | - |
| dc.date.issued | 2021 | - |
| dc.identifier.uri | https://doi.org/10.5109/4491843 | - |
| dc.identifier.uri | http://repository.futminna.edu.ng:8080/jspui/handle/123456789/26931 | - |
| 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, 08 (03), 667-672 | en_US |
| dc.relation.ispartofseries | ;08 (03), 667-672 | - |
| dc.subject | Bird control; computational fluid dynamics; structural analysis; surveillance; 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: | Mechanical Engineering | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Structural Integrity Study for a Quadcopter Frame to Be.pdf | 304.08 kB | Adobe PDF | View/Open |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.