Design And Simulation Of Rc Cargo Airplane


EOI: 10.11242/viva-tech.01.05.110

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Citation

Hitesh G Kateliya , Chetan S Manke, Riddhi N Kuwalekar, Shubham D Gaonkar, "Design And Simulation Of Rc Cargo Airplane", VIVA-IJRI Volume 1, Issue 5, Article 110, pp. 1-6, 2022. Published by Computer Engineering Department, VIVA Institute of Technology, Virar, India.

Abstract

The aircraft was first invented by wright brothers. In Previous 10 years, number of passengers death per kilometre increases. To overcome these problems, new innovation was done by scientist which was unmanned aerial vehicle (UAV). UAV is used in many sector such as military, surveillance of geographical boundary, agricultural, cargo transportation. In India UAV is refused in public sector, but most probably it is used in military because there is no human interference. So there is no risk to soldier life. This was achieved by choosing the optimum values of fuselage length, wingspan, elevator, rudder dimension and all up weight determined by a series of iterative analysis. The modelling can be done using the software Solid Works. The analysis of determining the parameters of the plane can be done using XFLR-5. This can be also confirmed by the method of computational fluid dynamics using commercial software ANSYS.

Keywords

RC plane, Fuselage, Wingspan, Elevator, Rudder, Drag Lift, Stall and angle of attack.

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