Design and Angle of Contact (AoA) analysis of Remote Control (RC) Aircraft

Authors

  • Chandra C Vijay Assistant Professor, Department of Mechanical Engineering, QIS College of Engineering & Technology, Ongole, Andhra Pradesh, India Author
  • Satish Kumar Assistant Professor, Department of Mechanical Engineering, QIS College of Engineering & Technology, Ongole, Andhra Pradesh, India Author
  • T Seshaiah Associate Professor, Department of Mechanical Engineering, QIS College of Engineering & Technology, Ongole, Andhra Pradesh, India Author

Keywords:

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

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.

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References

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Published

2022-12-30

Issue

Vol. 9 No. 6 (2022): International Journal of Innovative Research in Engineering & Management (Dec) 2022

Section

Articles

How to Cite

Design and Angle of Contact (AoA) analysis of Remote Control (RC) Aircraft . (2022). International Journal of Innovative Research in Engineering & Management, 9(6), 43–46. Retrieved from https://acspublisher.com/journals/index.php/ijirem/article/view/10665