Flow over airfoil

Objective: Introduction : Drag is defined as the force that acts in the direction opposite to the direction of motion `D = (Cd * rho *V^2 *A1)/2` Lift is defined as the force acting in the direction perpendicular to the direction of motion of the body `L = (Cl * rho *V^2 *A2)/2` Where, Cd and Cl are coefficients of drag and lift…