Aerodynamic Analysis of TEagle Eyes X-II Mini UAV by Using CFD

Authors

  • Itti Yuthayanon Aeronautical Engineering Department, Aeronautical Engineering and Aviation Technology Division, Academic Faculty, Navaminda Kasatriyadhiraj Royal Air Force Academy
  • Wanchai Jiajan Graduate School, Navaminda Kasatriyadhiraj Royal Air Force Academy
  • Thitiphun Vongkunghae Aeronautical Engineering Department, Aeronautical Engineering and Aviation Technology Division, Academic Faculty, Navaminda Kasatriyadhiraj Royal Air Force Academy

Keywords:

Aerodynamics, Stability, TEagle Eyes X-II Mini UAV, Computational Fluid Dynamics, CFD

Abstract

The objective of this paper is to analyze aerodynamic characteristics and aircraft stability of TEagle Eyes X-II mini UAV by using Computational Fluid Dynamics (CFD) in range of low Reynolds number about 500,000 - 800,000. TEagle Eyes X-II is designed to be able to fly according to the required performance and predetermined mission, which can take off by hand-launched or by using catapult and land by gliding and descending to the ground. The analysis results can confirm the trend of TEagle Eyes X-II capabilities, which are defined in the conceptual design process, one of the process of research, development and construction of mini UAV. More efficient operation in tactical missions will be obtained, and the design of mini UAV, which meets the operational requirements of intelligence, surveillance and reconnaissance missions will be acquired. In addition, the knowledge gained will continue to serve as information on the research and development of the Royal Thai Air Force's Mini UAV that can support other missions.

Author Biography

Itti Yuthayanon, Aeronautical Engineering Department, Aeronautical Engineering and Aviation Technology Division, Academic Faculty, Navaminda Kasatriyadhiraj Royal Air Force Academy

Wing Commander Assistant Professor Itti Yuthayanon Diplom-Ingenieur Univ. (Aerospace Engineering) Lecturer of Aeronautical Engineering Department, Aeronautical Engineering and Aviation Technology Division, Academic Faculty, Navaminda Kasatriyadhiraj Royal Air Force Academy

References

1. กองทัพอากาศ. (2563). ยุทธศาสตร์กองทัพอากาศ 20 ปี (พ.ศ.2561 - 2580). ฉบับปรับปรุง ปี พ.ศ.2563.
2. Jiajan, W., Tongsawang, K. and Sukuprakan, N. (2017). Aerodynamic Study and Analysis of Airfoils and Wings of Tailless Mini-UAV. NKRAFA Journal of Science and Technology, 13: 45-56.
3. Jiajan, W., Tongsawang, K. and Keawchay, K. (2018). Aerodynamic Investigations of Tailless Mini UAV by Using Subsonic Wind Tunnel. NKRAFA Journal of Science and Technology, 14: 77-85.
4. Coleman, H.W. and Steele, W.G. (1989). Experimentation and Uncertainty Analysis for Engineers. New York: John Wiley & Sons.
5. Versteeg, H.K. and Malalasekera, W. (2007). An Introduction to Computational Fluid Dynamics. Second Edition. London: Pearson Education Limited.
6. Jamshed, S. (2015). Using HPC for Computational Fluid Dynamics, A Guide to High Performance Computing for CFD Engineers. Oxford: Elsevier Inc.
7. Islam, S., Samsuzzoha, Ara, S., Islam, N. (2013). Unsteady Solutions of Thermal Boundary Layer Equations by using Finite Difference Method. Annals of Pure and Applied Mathematics. 3(2): 142-154.
8. Bertin, J.J. and Cummings, R.M. (2014). Aerodynamics for Engineers. Sixth Edition. London: Pearson Education Limited.

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Published

2021-06-30

How to Cite

[1]
I. Yuthayanon, W. Jiajan, and T. Vongkunghae, “Aerodynamic Analysis of TEagle Eyes X-II Mini UAV by Using CFD”, NKRAFA J.Sci Technol., vol. 17, no. 1, pp. 19–31, Jun. 2021.

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Section

Research Articles