International Research Journal of Innovations in Engineering and Technology - IRJIET International Open Access, Monthly, Peer Reviewed, Reputed Journal ISSN (online): 2581-3048

Impact Factor (2025): 6.9

DOI Prefix: 10.47001/IRJIET

Analysis of the Aerodynamics Parameters and Design of the Fixed Wing for the Drone

Manuel Alejandro Lira MartinezUniversidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, MéxicoArturo Paz PerezUniversidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, MéxicoChristian Aguirre TerrazasUniversidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, MéxicoAbril Abigail Solis SalazarUniversidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, MéxicoJulio Cesar Cuellar MataUniversidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, México

Vol 5 No 4 (2021): Volume 5, Issue 4, April 2021 | Pages: 87-96

International Research Journal of Innovations in Engineering and Technology

OPEN ACCESS | Research Article | Published Date: 16-04-2021

doi Logo doi.org/10.47001/IRJIET/2021.504014

pdf iconFull Text PDF
Abstract

The capacity of a wing to generate lift force is determined by the lift and drag coefficients produced by the effects of the airflow path along the selected airfoil and surface geometry. On this research, a methodology has been developed, based on the System Life Cycle management tool and mathematical models to perform a theoretical, computational, and experimental aerodynamic analysis in order to design and model a fixed wing for an UAV.

Keywords

Aerodynamic analysis, design and model, fixed wing, Unmanned Aerial Vehicle


Citation of this Article

Manuel Alejandro Lira Martinez, Arturo Paz Perez, Christian Aguirre Terrazas, Abril Abigail Solis Salazar, Julio Cesar Cuellar Mata, “Analysis of the Aerodynamics Parameters and Design of the Fixed Wing for the Drone” Published in International Research Journal of Innovations in Engineering and Technology - IRJIET, Volume 5, Issue 4, pp 87-96, April 2021. Article DOI https://doi.org/10.47001/IRJIET/2021.504014

Licence Copyright (c) 2026 International Research Journal of Innovations in Engineering and Technology creative common licence This work is licensed under Creative common Attribution Non Commercial 4.0 Internation Licence
References
  1. M. H. Sadraey, “Aircraft Design: A Systems Engineering Approach”, John Wiley & Sons, Ltd., 2013.
  2. Technical Commission, "Regular Class Official Contest Rulesl", SAE Aero Design, México, Revision NC, 2018.
  3. M. Simons, “Model Aircraft Aerodynamics”, Argus Books, 1993.
  4. S. G. Kontogiannis, J. A. Ekaterinaris, “Design, performance evaluation and optimization of a UAV”, Aerospace Science and Technology, 29, pp. 339-350, 2013.
  5. P. Raymer, “Aircraft Design: A Conceptual Approach”, American Institute of Aeronautics and Astronautics Inc., 1992.
  6. G. E. García, J. Nevárez, G. Fernández, X. Chávez, K. Olivares, “AerodynamicandControlAnalysis for anUnmannedAircraft”,  IOS Press, pp. 143-150, 2017.
  7. J. D. Anderson “Introduction to Flight”, McGraw-Hill Series in Aeronautical and Aerospace Engineering, 1989.
  8. H. Abbott, A. E. Von Doenhoff, “Theory of wing sections, Including a Summary of Airfoil Data”, Dover Publications, 1959.
  9. J. D. Anderson, “Aircraft Performance and Design”, WCB/McGraw-Hill, 1999.

Copyright @ 2026 IRJIET. All Right Reserved.

Licensed underCreative Commons Attribution 4.0 International License.