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Project

NACA Airfoil Simulation

PPrashant Chauhan8 Feb 2019
CFDSOLIDWORKS

Objective: 1.Objective The objective of this project is to do 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…

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