Find frontal area of parachute-skydiver-s terminal velocity


A certain parachute has a drag coefficient of 1.5. If the parachute and the skydiver together weigh 225 lb, what should the frontal area of the parachute be so the skydiver's terminal velocity is 15 mph when approaching the ground? Is it reasonable to neglect the buoyant force that is present?

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Mechanical Engineering: Find frontal area of parachute-skydiver-s terminal velocity
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