Write a computer program or script to compute the power required as a function of airspeed at a specific altitude. For the aircraft in Problem 2: (a) Use your computer program/script to compute (and plot on the same axes) the power required for level, unaccelerated flight and the power available as a function of airspeed (100 to 1,000 ft/s) for geopotential altitudes of 0 ft, 15,000 ft, and 30,000 ft. Assume that the thrust available is proportional to the change in air density, i. e.