Optimization of Wing Rib Configurations for Improved Aerodynamic Performance: A Computational Study

Abstract

Abstract: This research paper presents a computational study on the optimization of wing ribs configurations for improved aerodynamic performance. The wing ribs play a crucial role in supporting the wing's shape and contour, and their design is critical for achieving optimal flight performance. An aircraft's wing is a complex structure because of the complicated way it responds to different loads and manoeuvres. The main objective of this study is to develop a more efficient and optimized rib structure that can improve the aerodynamic performance of the wing, specifically by reducing drag and increasing lift. The study uses computational fluid dynamics (CFD) simulations to analyze the aerodynamic performance of different wing rib configurations. The simulations are performed on a representative wing model, and different rib designs are evaluated to determine their impact on the overall aerodynamic performance. The results of the study demonstrate that the optimized rib structure can significantly improve the aerodynamic performance of the wing, with a reduction in drag and an increase in lift. The study also highlights the potential benefits of using computational techniques for designing and optimizing aircraft components, such as reducing design time and cost, improving accuracy, and enabling rapid prototyping. The findings of this study are expected to contribute to the development of more efficient and effective aircraft design processes, benefiting both the aviation sector and the public.