Technical Papers - SAE Mobilus

SAE Technical Papers are written and peer-reviewed by experts in the automotive, aerospace, and commercial vehicle industries and provide the latest advances in technical research and applied technical engineering information.

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Design and Multi-Parametric Computational Investigations on the Propulsive System of a Pentacopter UAV2025-28-0181To be published on 02/07/2025
This work deals with the design and multi-parametric investigation on the uniquely designed propeller for a Pentacopter Unmanned Aerial Vehicle (UAV). The primary design data, secondary design data and performance coefficients such as diameter of the propeller, pitch angle, chord length, lift coefficient are determined through standard analytical approach. About ten different airfoils such as NACA 2412, NACA 4109, NACA 4312, NACA 4409, NACA 4415, NACA 5317, NACA 6409, NACA 6412, NACA 23024, NACA 25012 with 13 Reynolds Number and an Angle of Attack (AOA) of 20 ranges between -5 to 15 degrees are compared in order to design the propellers. The lift coefficient and drag coefficient values of ten different airfoils using the 13 Reynolds Number and the 20 AOA are acquired from the X-foil software. Based on the effect of high lift to drag ratio (L/D), three advanced airfoils are chosen among ten relevant airfoils. The shortlisted airfoils by means of high L/D ratio provided are as follows
Arumugam, ManikandanSolaiappan, Senthil KumarVeeraperumal Senthil Nathan, JananiPriyadharshiniKulandaiyappan, Naveen KumarMadasamy, Senthil KumarSolaiappan, Senthil KumarVeeraperumal Senthil Nathan, JananiPriyadharshiniKulandaiyappan, Naveen KumarMadasamy, Senthil KumarStanislaus Arputharaj, BeenaL, NatrayanRaja, Vijayanandh
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