Experimental Study on Relation of Small UAV Propeller Thrust Generation and The Mouth-Ring

In this study, the main focus is to study the thrust generation of various propeller blade width-spans with the mouth-ring application. By using the parameter, the thrust were calculated based on the value of velocity, voltage and RPM. The testing was performing in three different width-span that ar...

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Bibliographic Details
Published in:IOP conference series. Materials Science and Engineering 2018-11, Vol.429 (1), p.12079
Main Authors: Othman, M. N. K., Razlan, Z M, Muhamad Azmi, M S, Zunaidi, I, Wan, W K, Shahriman, A B, Hashim, M S M, Faizi, M K, Ibrahim, I, Kamarrudin, N S
Format: Article
Language:English
Subjects:
Mathematical analysis
Propeller blades
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Summary:In this study, the main focus is to study the thrust generation of various propeller blade width-spans with the mouth-ring application. By using the parameter, the thrust were calculated based on the value of velocity, voltage and RPM. The testing was performing in three different width-span that are; 10mm, 8mm and 5mm. There are also variable that be tested that cover the reducing the diameter of mouth-ring from 36 mm to 32mm. In addition, if compared the gaps and different position proved that centre position gives better thrust. Furthermore, the application of mouth-ring is evaluated to be good base on this study
ISSN:1757-8981
1757-899X
1757-899X
DOI:10.1088/1757-899X/429/1/012079