Evaluación del desempeño aerodinámico de dos perfiles de ala tipo anular para una aeronave mediante simulaciones de dinámica de fluidos computacional (CFD)

Abstract

This project aims to evaluate the aerodynamic performance of two annular wing profiles for aircraft using Computational Fluid Dynamics (CFD) simulations. The goal is to address the limitations in aerodynamic efficiency and high fuel consumption associated with conventional wing designs. The aviation industry faces significant challenges in improving aerodynamic efficiency and reducing fuel consumption, especially with the increase in air traffic and operational costs. Although conventional wings have been optimized, they still present limitations in minimizing drag and maximizing lift under varying flight conditions. In this context, annular wings emerge as an innovative design with the potential to overcome these limitations. However, their aerodynamic behavior has not been fully studied, limiting knowledge about their feasibility and capacity to enhance aircraft efficiency. Through CFD simulations, this project will analyze and compare the aerodynamic behavior of two annular wing profiles with different leading and trailing edge geometries. Simulations will be conducted under various altitude conditions to assess key aspects such as lift, drag, airflow patterns around the wings, and flight stability. The results could contribute to the development of new technologies and innovative concepts in aircraft design, exploring alternative solutions for more efficient and sustainable aviation.