Matlab

5) The surface of many airfoils can be described with an equation of the form JV Thickness max where t is the maximum thickness as a fraction of the chord length c (e.g., maxct). Given that c - 1 m and t - 0.2 m, the following values for y have been measured for a particular airfoil: 0.5 0.7 x(m)11 0.15 | 0.35 y (m)0.08909 0.099140.088230.061070.03421 0.85 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.)