Flow over a Naca Airfoil

Objective: Aim:Model the flow over a NACA0017 airfoil For the angle of attacks 0,2,4,6,8,10 compare the lift and drag forces Inroduction: The NACA airfoils are airfoil shapes for aircraft wings developed by the (NACA). The shape of the NACA airfoils is described using a series of digits following the word \"NACA\". The parameters…