Create a script in Octave that can do the following

.One key performance characteristic in the design of arn aircraft is the drag coefficient as it directly affects fuel efficiency Drag on an airplane is a complex phenomena to model as it is a combination of surface properties of the aircraft (skin friction), fluid properties (air), and flow patterns. Because of this, the drag coefficient must be determined experimentally . While the drag coefficient is not constant for all wind speeds it can be taken as a constant for low speeds (less than 200 mph) For this assignment: 1. Write a script file named "drag.m" to calculate the drag coefficient, Cd, based on the equation and measured parameters below: D, the drag force, at 20,000 N p, the air density, at 1 x 10-6 kg/m V, the aircraft velocity, at 100 mph A, the surface area, at 1 m2 2 D 2. Plot the drag force for at least 10 wind speeds between 0 and 200 mph. .One key performance characteristic in the design of arn aircraft is the drag coefficient as it directly affects fuel efficiency Drag on an airplane is a complex phenomena to model as it is a combination of surface properties of the aircraft (skin friction), fluid properties (air), and flow patterns. Because of this, the drag coefficient must be determined experimentally . While the drag coefficient is not constant for all wind speeds it can be taken as a constant for low speeds (less than 200 mph) For this assignment: 1. Write a script file named "drag.m" to calculate the drag coefficient, Cd, based on the equation and measured parameters below: D, the drag force, at 20,000 N p, the air density, at 1 x 10-6 kg/m V, the aircraft velocity, at 100 mph A, the surface area, at 1 m2 2 D 2. Plot the drag force for at least 10 wind speeds between 0 and 200 mph