User:Eas4200c.f08.vqcrew.c/Homework 3\my\

MATLAB Question
The task for the MATLAB portion of the HW report involves plotting an arbitrary NACA airfoil, finding the average area of the airfoil, and locating the airfoil's area centroid.

Using the following input (in accordance with the syntax presented in the code header), the code generates Figure ##, a graph of the NACA 2415 airfoil with a cross-hair at the centroid.

 >> abar(1,1,2,4,15,1000,[0;0])

The average area of the airfoil is 0.101 square chord units

The centroid is located at (0.420,0.016) chord units

>>