• JV Muruga lal Jeyan
• Rajesh Thapa Chhetri
• Prem sai Thota
• Prashant Shrestha
• Shaik Sharuk Pasha

This paper aims to present the results of aerodynamic calculation of the aircraft in tricopter with 2 fixed brushless and a servo attached motor at the rear side. A presented unmannedaerial vehicle is one of two types of tricopter UAVs, but presented and analyzed in basic level. The aircraft is equipped with a pair of fixed rotors mounted on the tips of the front and a servo attached rotor to the rear wings/arms. The main goal of the presented research was to research, design and analyze a rarer kind of the aircraft. Moreover, the studied model or design is also supposed to be manufactured later. Methodology/approach – The Solid Works was used to design and assemble the parts/components of the UAV. Detailed study of tricopter types and components along with mathematical logic was conducted by the team in order to learn about the tri rotor UAVs. Findings – The result obtained from the study includes the functioning along with the given components. Not only that, it covers the mechanical forces that are acting on our UAV. The influence of the angle of attack, sideslip angle and the change of angle of servo motor was briefly investigated. New design of tricopter is also provided. Practical implications – Presented results could be very useful in the computation of dynamic stability of unconventional aircraft. Moreover, results could be slightly helpful during designing the aircraft in the tandem wing configuration.

UAV, Tri Prop, Dynamic Pressure, Design Of aircraft, Drons

"Design and development of a tri-pro UN manned Arial vehicle Concept for commercial application", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 3, page no.2459-2473, March-2021, Available :http://www.jetir.org/papers/JETIR2103306.pdf

"Design and development of a tri-pro UN manned Arial vehicle Concept for commercial application", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 3, page no. pp2459-2473, March-2021, Available at : http://www.jetir.org/papers/JETIR2103306.pdf