In matlab

oWnls, and use MAT- LAB to solve the equations.) 5) The surface of many airfoils can be described with an equation of the form Thickness tc 0.2 o where t is the maximum thickness as a fraction of the chord length c (e.g., max ct). Given that c 1m and t-0.2m, the following values for y have been measured for a particular airfoil: 0.7 0.85 x (m) 0.15 0.35 0.5 y (m) 0.08909 09914 0.08823 0.06107 0.03421 Determine the constants ao, ai , a2, , and a4 . (Write a system of five equa- tions and five unknowns, and use MATLAB to solve the equations.)