Question: (In matlab) Write a function to calculate the aerodynamic drag on a body using the equation where Co is the drag coefficient A is the

(In matlab)

(In matlab) Write a function to calculate the aerodynamic drag on abody using the equation where Co is the drag coefficient A is

Write a function to calculate the aerodynamic drag on a body using the equation where Co is the drag coefficient A is the frontal area of the body p is the density of air V is the velocity

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