Computational assessment of winglet-induced variations in pressure coefficients on NACA 4418 aircraft wings

This study presents a computational analysis of the effects of winglets on the aerodynamic performance of NACA 4418 aircraft wings, focusing on the variations in pressure coefficients. Using Computational Fluid Dynamics (CFD) simulations, we evaluated the aerodynamic behavior of NACA 4418 wings unde...

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Bibliographic Details
Main Authors: Md. Abdullah, Mohammad Zoynal Abedin
Format: Article
Language:English
Published: SAGE Publishing 2025-01-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/16878132251314329
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