Project

Flow over an Airfoil - CFD using SOLIDWORKS

Objective: Abstract In this Project, CFD analysis of the two-dimensional subsonic flow over a NACA 0017 airfoil at various angles of attack and compare the lift and drag force. The geometry of the airfoil is created using SOLIDWORKS. CFD analysis is carried out using Flow Simulation Wizard at various angles of attack from 0°…

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