IN C++

Flight-Path Angle (degrees) Coefficient of Lift -0182 -0.056 0.097 0.238 0.421 0.479 0.654 0.792 0.924 1.035 1.076 1.103 1.120 1.121 1.121 1.099 1.059 6 10 14 15 17 20 Assume that we would like to use linear interpolation to determine the coefficient of lift for additional flight-path angles that are between -4 degrees and 21 degrees. Write a program that allows the user to enter the data for two points and a flight-path angle between those points. The program should then compute the corresponding coefficient of lift