An object that is falling through the atmosphere
is subjected to two external forces. The
first force is the gravitational force,
expressed as the
weight
of the object, and the second force is the aerodynamic
drag of the object.
The weight equation
defines the weight W to be
equal to the mass m of the object times the gravitational acceleration
g:
W = m * g
the value of g is 9.8 meters per square second on the surface of the
earth. The gravitational acceleration decreases with the square of
the distance from the center of the earth. But for most practical
problems in the atmosphere, we can assume this factor is
constant. If the object were falling in a vacuum, this would be the
only force acting on the object. But in the
atmosphere, the motion of a falling object is opposed by the aerodynamic
drag. The drag
equation tells us that drag D is equal to a
drag coefficient Cd
times one half the air density r
times the velocity V squared
times a reference area A
on which the drag coefficient is based:
D = Cd * .5 * r * V^2 * A
The motion of any moving object can be described by Newton's
second law of motion, force F
equals mass m times acceleration a:
F = m * a
We can do a little algebra and solve for the
acceleration of the object in terms of the net external force and the
mass of the object:
a = F / m
Weight and drag are forces which are
vector quantities.
The net external force is then equal to the
difference
of the weight and the drag forces:
F = W - D
The acceleration of the object then becomes:
a = (W - D) / m
The drag force depends on the square of the velocity.
So as the body accelerates its velocity and the drag increase.
It quickly reaches a point
where the drag is exactly equal to the weight. When drag is equal to
weight, there is no net external force on the object,
and the acceleration becomes zero. The object
then falls at a constant velocity as described by
Newton's first law of motion.
The constant velocity is called the terminal
velocity.
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