The function EGA118_M2_Q2.m is intended to calculate the values of the coefficient of lift, CL. and the coefficient of drag, CD, from the following equations: CL=a(0)CD=CD0+KCL2 There are errors in the function that need to be corrected for the function to work correctly. Please complete the following tasks. - Correct the function. - Adjust the function so that it will work if the angle of attack, the alpha variable, is an array. All other input arguments will remain single valued. - Write a script in a separate file that produces a plot of CL against CD when a=0.1, 0=2.5,CD0=0.025 and K=0.034 for angles of attack, , from -12 to 10 degrees. [15 marks]function CL and CD (a,alpha0,C D0,K) CL=a(alphaalpha0); CD=CD0+kCL2; end.