Abstract: This workflow includes study of airfoils for BOEING 737, NACA 2412, EPPLER 1098. Wings are created using these airfoils. This consists of a CAD model of the wing with and without dimples which are prepared using Solidworks and its analysis is done in Ansys fluent. Computational Fluid Dynamics [CFD] is carried out on all three wings with the boundary conditions as the original.

Keywords: Airfoil, BOEING 737, NACA 2412, EPPLER 1098, Dimples

| DOI: 10.17148/IARJSET.2022.9825