Análisis Aerodinámico de la Aeronave usb Aero Mediante Dinámica de Fluidos Computacional

Authors

  • Juan Gabriel Sanchez Ocampo Universidad De San Buenaventura Sede Bogotá - Colombia.
  • Jordy Francisco Tamayo Andrade Universidad De San Buenaventura Sede Bogotá - Colombia.
  • Sergio Andres Lopez Aragon Universidad De San Buenaventura Sede Bogotá - Colombia.
  • Rafael Mauricio Cerpa Bernal Universidad De San Buenaventura Sede Bogotá - Colombia.

Keywords:

CFD, aircraft, Lift and drag coefficients

Abstract

The present research study presents the results of the aerodynamic analysis of a USB AERO aircraft using computational fluid dynamics (CFD) in operational conditions of cruise flight at an angle of attack of 3.5
degrees. The ANSYS FLUENT computational tool was used, with which the
lift, drag and longitudinal momentum coefficients were determined. Additionally, the aircraft was analyzed at different angles of attack in order to determine aerodynamic characteristics such as the highest lift coefficient
and the loss angle, in addition to establishing the maximum aerodynamic
efficiency.

Published

2020-04-25

How to Cite

Sanchez Ocampo , J. G. ., Tamayo Andrade, J. F. ., Lopez Aragon, . S. A. ., & Cerpa Bernal, R. M. . (2020). Análisis Aerodinámico de la Aeronave usb Aero Mediante Dinámica de Fluidos Computacional. Tecciencia, 15(28), 55–66. Retrieved from https://tecciencia.ecci.edu.co/index.php/TECCIENCIA/article/view/33