Dynamics of Uniform Circular Motion Uniform Circular Motion Centripetal Acceleration Centripetal Force Satellites in Circular Orbits Vertical Circular Motion
Uniform circular motion is the motion of an object traveling at a constant speed on a circular path Period (T) is the time required to make one complete revolution V = 2 r / T Magnitude of the velocity vector is constant, however, the vector changes direction and is therefore accelerating. This is known as centripetal acceleration.
Magnitude: The centripetal acceleration can be calculated by the following A c = v 2 /r Direction: The centripetal acceleration vector always points toward the center of the circle and continually changes direction as the object moves. **The centripetal acceleration is smaller when the radius is larger Pg 155 #1, 3, pg 156 #1, 5, 9
Newton’s second law indicates that when an object accelerates there must be a net force to create the acceleration. The centripetal force points in the same direction as the acceleration (toward the center) and can be calculated as follows: F c = mv 2 /r Name given to the net force required to keep an object of mass m, moving at speed v, on circular path of radius r. Pg 155 #7, pg 156 #13, 15, 21
There is only one speed that a satellite can have if the satellite is to remain in orbit with a fixed radius. For a given orbit, a satellite with a large mass has exactly the same orbital speed as a satellite with a small mass. See pg ex 9 Pg 155 #11, pg 158 #31, 33
There are 4 points in a vertical circle where the centripetal force can be identified. The centripetal force is the net sum of all of the force components oriented/pointing toward the center of the circle. EX pg 151 Pg 155 #15, pg 158 #41, 43, 45, pg 159 # 59