HELP WITH MATLAB!!!

URGENT

Problem 4.3 When calculating the lift and drag on an airfoil in an airstream, it is convenient to describe the surface shape in polar coordinates (r, 6). On the following page, you will find the coordinates of several points on the surface of a Clark Y-14 airfoil. Write a MATLAB program to do the following: Store the airfoil shape (in polar coordinates) to variable(s). Convert the points to Cartesian coordinates (x,y). Generate a plot of these (x,y) points o de both markers and lines on the plot. o Label the axes appropriately. Be sure to include the units. o Your plot should be in a different figure window than the plot from Problem 4.2