IJIREM

Abstract

In this paper, the design of a prototype of Remote Control (RC) aircraft is discussed. It is important and interesting to learn about the workings, terminology, factors affecting to flight, construction, application, and advantage of the aircraft. Also, studied about the designing aeronautics formula rules and analytical equations of aircraft lift force and drag force of a RC airplane for AOA analysis. In addition, aerodynamic performance is carried out on the airfoil type wing to determine the drag and lift forces at maximum speed.

Keywords

RC Airplane, Design, 3D Modeling, AOA, Drag Force, Lift Force, Analytical formulas

Reference

S. S Hegde , S.Nayak , Kishan R, N.Chavan , A Systematic Approach for Designing, Analyzing and Building a Model RC Plane, International Journal of Engineering Research & Technology (IJERT) Vol. 3 Issue 12, December-2014, ISSN: 2278-0181.
Ryan B. eorge et al, A differentially driven flapping wing mechanism for force analysis and trajectory optimizationâ€Ÿ, International journal of micro air vehicles - Vol 4, March 2012.
Harish M, S. Narayanan N.A. Kumar G, Subramani J. Design, Fabrication and Aerodynamic Analysis of RC Powered Aircraft Wing, International Research Journal of Engineering and Technology (IRJET) Volume: 09 Issue: 07 , July 2022, e-ISSN: 2395-0056.
C.Rakesh, S. Kumar N, Design and Analysis of Solar Powered RC Aircraft, The International Journal Of Engineering And Science (IJES) , Volume 4 , Issue 12 , PP -29-41, 2015 , ISSN (e): 2319 – 1813.
DoÄŸru M.H., Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles. Çukurova University Journal of the Faculty of Engineering and Architecture, In Press.2017
S.K.Murthy, S. J.shankar, S.V.Rao, R. Krishna T S, S.G .Nyamannavar. CFD Analysis of An RC Aircraft Wing, International Journal of Mechanical and Production Engineering, Volume- 2, Issue-9, Sept.-2014, ISSN: 2320-2092.
B.Sweeten, CFD analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis software, Aerospace Engineering, Graduate Faculty of the University of Kansas, April 27, 2010.
C. Kim, J.Chung, Aerodynamic Analysis of Tilt-Rotor Unmanned Aerial Vehicle with Computational Fluid Dynamics, Journal of Mechanical Science and Technology (KSME Int. J.), Vol. 20, No.4, pp. 561-568, 2006..
M. A Azlin, C.F.M Taib, S. Kasolang et.al, CFD Analysis of Winglets at Low Subsonic Flow, Proceedings of the World Congress on Engineering 2011 Vol I, July 6 - 8, 2011.
N. Ullah, A A Riaz, M.Z.Zahir et.al. Design, Fabrication and Analysis of Light Weight Unmanned Air Vehicle (UAV). Journal of Mechanical Engineering Research and Developments 44(11):314-326.

Cites this article as

[Vijay Chandra.C, Satish Kumar, T. Seshaiah (2022), Design and Angle of Contact (AoA) analysis of Remote Control (RC) Aircraft, International Journal of Innovative Research in Engineering & Management (IJIREM), Vol-9, Issue-6, Page No-43-46], (ISSN 2347 - 5552). www.ijirem.org