Design and Analysis of Humanitarian Aid Delivery RC Aircraft


Authors : Sumit Dhage, Rushikesh Kumbhar, Abhijeet Gaikwad, Abhijeet Pardeshi

Volume/Issue : Volume 4 - 2019, Issue 8 - August

Google Scholar : https://goo.gl/DF9R4u

Scribd : https://bit.ly/2lAIt6c

A radio-controlled aircraft is an unmanned aerial vehicle operated through a trans-receiver module – one located at the controller’s end, other inside the aircraft. The following section discusses an RC aircraft mirroring a miniature cargo aircraft, the notable features being the glow-plug engine and data acquisition system (DAS) using an altimeter and first-person view (FPV) camera. The RC aircraft is equipped to perform tasks simulating payload airdrops and carrying stationary cargo. A RC aircraft poses similar engineering problems as involved in designing large scale aircraft, albeit at lower speeds. The airworthiness of a RC aircraft is established during the conceptualization, design and modelling, construction, assembly, and testing phases. Softwares such as NX Cad 12.0, ANSYS-Fluid, and XFLR5 were used while developing an airworthy aircraft. Reinforcements of Carbon-fibre during assembly were integrated to make the structure light and sturdy.

Keywords : Lift, Drag, Aspect Ratio, Angle of Attack, Stall.

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