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

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.

Country : Mexico

1 Manuel Alejandro Lira Martinez2 Arturo Paz Perez3 Christian Aguirre Terrazas4 Abril Abigail Solis Salazar5 Julio Cesar Cuellar Mata

  1. Universidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, México
  2. Universidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, México
  3. Universidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, México
  4. Universidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, México
  5. Universidad Autónoma de Ciudad Juárez. Ave. Del Charro 450 N Cd. Juárez, Chih. CP 32310, México

IRJIET, Volume 5, Issue 4, April 2021 pp. 87-96

doi.org/10.47001/IRJIET/2021.504014

Full Paper
Download

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 @ 2026-2017 IRJIET. All Right Reserved.

Developed by Byzero Technologies