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http://repository.futminna.edu.ng:8080/jspui/handle/123456789/18632Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Sulaiman, I. | - |
| dc.contributor.author | Alkali, B. | - |
| dc.contributor.author | Adedipe, O. | - |
| dc.contributor.author | Salihu, B. A. | - |
| dc.contributor.author | Abdullahi, Aliyu Alhaji | - |
| dc.contributor.author | Ibrahim, A. G. | - |
| dc.date.accessioned | 2023-05-04T16:15:53Z | - |
| dc.date.available | 2023-05-04T16:15:53Z | - |
| dc.date.issued | 2020-12-20 | - |
| dc.identifier.uri | http://repository.futminna.edu.ng:8080/jspui/handle/123456789/18632 | - |
| 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 shows promising results as the stress built up due to the loads applied are within the safe range | en_US |
| dc.language.iso | en | en_US |
| dc.subject | Quadcopters | en_US |
| dc.subject | Structure | en_US |
| dc.subject | Analysis | en_US |
| dc.title | Preliminary Structural Integrity Investigation for Quadcopter Frame to be Deployed for Pest Control | en_US |
| Appears in Collections: | Mechanical Engineering | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Sulaiman et al 2020.pdf | 673.57 kB | Adobe PDF | View/Open |
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