Design and numerical analysis of five blade propeller for a drone

Shanmugam, Yuvaraj; Renald, Thomas; Jukna, Artūras; Rathnaraj, J. David; Nallamani, M.; Kaviyarasan, P.

Use this URL to cite this publication: https://hdl.handle.net/20.500.14911/139806

Design and numerical analysis of five blade propeller for a drone

Details

Publication Type (CRIS)

Straipsnis Scopus duomenų bazėje / Article in Scopus database (S1b)

Publication Type (eLABa)

Straipsnis Scopus DB / Scopus DB article (S2)

VILNIUS TECH Research Priorities and Topics

Fizinių, technologinių ir ekonominių procesų matematiniai modeliai / Mathematical models of physical, technological and economic processes (FM0101)

Lithuanian Intelligent Specialization

Transportas, logistika ir informacinės ir ryšių technologijos (IRT) / Transport, logistic and information and communication technologies (L106)

Author(s)

Author	Affiliation
Shanmugam, Yuvaraj	Sri Ramakrishna Engineering College
Renald, Thomas	Sri Ramakrishna Engineering College
Jukna, Artūras	Fizikos katedra / Department of Physics (1020)
Rathnaraj, J. David	Sri Ramakrishna Engineering College
Nallamani, M.	Sri Ramakrishna Engineering College
Kaviyarasan, P.	Sri Ramakrishna Engineering College

Title

Design and numerical analysis of five blade propeller for a drone

[en]

Yuvaraj Shanmugam, Thomas Renald, Artūras Jukna, J. David Rathnaraj, M. Nallamani, P. Kaviyarasan

Is part of

International Journal of Engineering and Advanced Technology (IJEAT)

Published In

Year	Volume	Issue	Start Page	End Page
2019	8	2S2(25)	116	119

Publisher

Bhopal : Blue Eyes Intelligence Engineering & Sciences Publication (BEIESP)

Publisher (trusted)

Blue Eyes Intelligence Engineering & Sciences Publication (BEIESP)

Referenced in Database(s)(DBs)

Index Copernicus

INSPEC

SCOPUS

Extent

p. 116-119

URI

URI	Access Rights
https://hdl.handle.net/20.500.14911/139806
https://www.ijeat.org/portfolio-item/B10250182S219/	Viso teksto dokumentas (atviroji prieiga) / Full Text Document (Open Access)

Cited references

Science / Art Area

Gamtos mokslai / Natural Sciences (N)

Field of Science / Art

Fizika / Physics (N002)

Medžiagų inžinerija / Materials engineering (T008)

Keywords (en)

Abstract (en)

It is a major problem in UAVs to have a better stability in gusty winds and obtaining uniform thrust depend on the various directional and Aerobatic operations. Hence, we have fabricated an X4 model Drone with the existing propeller blade profiles of standard size. Its performance was measured and stability criteria specified by varying the pitch shows that the span parameters of the propeller and the stability can be improved. We designed a propeller and mounted in the fabricated Drone for the real time measurements of the stability.The stability of the Drone was increased by varying the propeller design. The analysis of the propeller blade was performed in Open FOAM platform with the maximum of 10000 rpm.