Final answer:
To find the drag coefficient in this scenario, we can use the equation for drag force: FD = 0.5 * ? * A * v^2, where FD is the drag force, ? is the drag coefficient, A is the cross-sectional area, and v is the velocity.
Step-by-step explanation:
To find the drag coefficient in this scenario, we can use the equation for drag force: FD = 0.5 * ? * A * v^2, where FD is the drag force, ? is the drag coefficient, A is the cross-sectional area, and v is the velocity. First, we need to convert the terminal velocity of 99 mi/h to ft/s, which is 145.2 ft/s. We can then rearrange the equation to solve for ?:
? = (2 * FD) / (A * v^2)
Substituting the values given in the question, we have:
? = (2 * mg - FD) / (A * v^2)
Where m is the mass of the paratrooper, g is the acceleration due to gravity, and FD is the drag force. We can calculate the value of ? using this equation.