4.7  Uniform Circular Motion
A particle is in uniform circular motion if it travels around a circle or a circular arc at constant (uniform) speed. Although the speed does not vary, the particle is accelerating because velocity changes in direction.

Figure 4-19 shows the relationship between the velocity and acceleration vectors at various stages during uniform circular motion. Both vectors have constant magnitude, but their directions change continuously. The velocity is always directed tangent to the circle in the direction of motion. The acceleration is always directed radially inward. Because of this, the acceleration associated with uniform circular motion is called a centripetal (meaning “center seeking”) acceleration. As we prove next, the magnitude of this acceleration is

  (4-34)


where r is the radius of the circle and v is the speed of the particle.
Figure zoom  FIGURE 4-19   Velocity and acceleration vectors for uniform circular motion.
Velocity and Acceleration

In addition, during this acceleration at constant speed, the particle travels the circumference of the circle (a distance of ) in time

  (4-35)


T is called the period of revolution, or simply the period, of the motion. It is, in general, the time for a particle to go around a closed path exactly once.

Proof of Eq. 4-34

To find the magnitude and direction of the acceleration for uniform circular motion, we consider Fig. 4-20. In Fig. 4-20a, particle p moves at constant speed v around a circle of radius r. At the instant shown, p has coordinates and .
Figure zoom  FIGURE 4-20   Particle p moves in counterclockwise uniform circular motion. (a) Its position and velocity at a certain instant. (b) Velocity . (c) Acceleration .

Recall from Section 4-3 that the velocity of a moving particle is always tangent to the particle’s path at the particle’s position. In Fig. 4-20a, that means is perpendicular to a radius r drawn to the particle’s position. Then the angle that makes with a vertical at p equals the angle that radius r makes with the x axis.

The scalar components of are shown in Fig. 4-20b. With them, we can write the velocity as

  (4-36)

Now, using the right triangle in Fig. 4-20a, we can replace with and with to write

  (4-37)


To find the acceleration of particle p, we must take the time derivative of this equation. Noting that speed v and radius r do not change with time, we obtain

  (4-38)

Now note that the rate at which changes is equal to the velocity component . Similarly, , and, again from Fig. 4-20b, we see that and . Making these substitutions in Eq. 4-38, we find

  (4-39)

This vector and its components are shown in Fig. 4-20c. Following Eq. 3-6, we find
as we wanted to prove. To orient , we find the angle shown in Fig. 4-20c:
Thus, , which means that is directed along the radius r of Fig. 4-20a, toward the circle’s center, as we wanted to prove.

 Checkpoint 5
An object moves at constant speed along a circular path in a horizontal xy plane, with the center at the origin. When the object is at , its velocity is . Give the object’s (a) velocity and (b) acceleration at .


Sample Problem 4-10
“Top gun” pilots have long worried about taking a turn too tightly. As a pilot’s body undergoes centripetal acceleration, with the head toward the center of curvature, the blood pressure in the brain decreases, leading to loss of brain function.

There are several warning signs. When the centripetal acceleration is 2g or 3g, the pilot feels heavy. At about 4g, the pilot’s vision switches to black and white and narrows to “tunnel vision.” If that acceleration is sustained or increased, vision ceases and, soon after, the pilot is unconscious—a condition known as g-LOC for “g-induced loss of consciousness.”

What is the magnitude of the acceleration, in g units, of a pilot whose aircraft enters a horizontal circular turn with a velocity of and 24.0 s later leaves the turn with a velocity of ?
 KEY IDEA 
We assume the turn is made with uniform circular motion. Then the pilot’s acceleration is centripetal and has magnitude a given by Eq. 4-34 , where R is the circle’s radius. Also, the time required to complete a full circle is the period given by Eq. 4-35 .

Calculations: Because we do not know radius R, let’s solve Eq. 4-35 for R and substitute into Eq. 4-34. We find
Speed v here is the (constant) magnitude of the velocity during the turning. Let’s substitute the components of the initial velocity into Eq. 3-6:
To find the period T of the motion, first note that the final velocity is the reverse of the initial velocity. This means the aircraft leaves on the opposite side of the circle from the initial point and must have completed half a circle in the given 24.0 s. Thus a full circle would have taken . Substituting these values into our equation for a, we find

  (Answer)

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