Análisis Aerodinámico de la Aeronave usb Aero Mediante Dinámica de Fluidos Computacional
Keywords:
CFD, aircraft, Lift and drag coefficientsAbstract
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.
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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
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