Design, Fabrication and Aerodynamic Analysis of a RC Airplane

Abstract An internal receiver and a hand-held transmitter enable the remote operation of a (model) airplane, often known as an RC plane or airplane, to be operated remotely. The objective is to create a high-performance, stable, and maneuverable RC airplane maintaining an optimum AOA suitable for recreational and hobbyist use. Since the used electronic components are freely available in markets and do not require user programming, this paper did not focus on them. In this study, computational fluid dynamic (CFD) analysis was used to discuss wing shape, and control surface configuration to optimize lift, drag, and stability also calculated the optimum angle of attack which was found to be below 15 degrees. The N10 airfoil was taken into consideration for the wing design based on its asymmetrical shape for better lift and aerodynamic performance. Overall, this article provides valuable insights and guidelines for the design and development of RC airplanes, fostering advancements in this exciting field of aviation.

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Publication Details

Journal
Journal of Physics Conference Series
Published
2024-10-01
DOI
https://doi.org/10.1088/1742-6596/2856/1/012002
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
0.00
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article

Design, Fabrication and Aerodynamic Analysis of a RC Airplane

Md. Tanvir Ahmed, Durjoy Chandra Shil, Md Robin Mia, Nilotpala Bej
Journal of Physics Conference Series
Computational Fluid Dynamics and Aerodynamics
article

Design, Fabrication and Aerodynamic Analysis of a RC Airplane

Md. Tanvir Ahmed, Durjoy Chandra Shil, Md Robin Mia, Nilotpala Bej
article en

Abstract

Abstract An internal receiver and a hand-held transmitter enable the remote operation of a (model) airplane, often known as an RC plane or airplane, to be operated remotely. The objective is to create a high-performance, stable, and maneuverable RC airplane maintaining an optimum AOA suitable for recreational and hobbyist use. Since the used electronic components are freely available in markets and do not require user programming, this paper did not focus on them. In this study, computational fluid dynamic (CFD) analysis was used to discuss wing shape, and control surface configuration to optimize lift, drag, and stability also calculated the optimum angle of attack which was found to be below 15 degrees. The N10 airfoil was taken into consideration for the wing design based on its asymmetrical shape for better lift and aerodynamic performance. Overall, this article provides valuable insights and guidelines for the design and development of RC airplanes, fostering advancements in this exciting field of aviation.

Journal of Physics Conference SeriesVol. 2856(1)
KIIT University (IN)
Openalex Percentile: Top 80%
Computational Fluid Dynamics and Aerodynamics
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