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The lecture notes for lecture 34 of physics 1110, fall 2004. The topic covered in this lecture is elliptical orbits and potential energy. How to calculate the potential energy using newton's law of gravity and discusses the behavior of particles in elliptical orbits, including escape velocity and the energy of a circular orbit. The document also introduces the concept of rotational motion and rotational kinematics.
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Now we cannot use our centripetal acceleration formula, since the radius is not constant. Since the force will now change with distance between the sun and a planet (for example) this means the acceleration is not constant and we would need to solve differential equations to derive a solution. However, we can do an energy analysis if we use the potential energy U that comes from Newton’s law for gravity. By considering the work when moving an object m from ri to r (^) f while feeling the force from a planet with mass M, we can derive that the correct function is
This formula can be confusing. It just depends on the distance between the centers so it extends in all directions from a planet. Also it starts from a very negative number and grows with distance. Don’t be confused by considering the magnitude of U. At small r, it is very small (large magnitude and negative). Also, it appears to blow up to – infinity when r=0. But in fact, this never happens; the objects hit each other first and then we have additional contact forces to prevent them from going to r=0. Since it is a potential energy, we can always just imagine a ball “rolling” down the potential energy curve; it will roll towards r = 0 as it should, and potential energy grows the “higher” above the ground (greater r) you go.
The figure shows an energy diagram for this potential energy. Note that if we also plot a particle’s energy E as a constant at some value, there are 2 very different behaviors. If E > 0, then there is no turning
point and the particle escapes. If E < 0, it is trapped, and that means it can never go greater than a certain distance from the mass M. This is what an orbit is! As usual, we see that when the particle gets close to M, it’s kinetic energy grows, and when it moves away it gets slow. So in an elliptical orbit, the planet speed near the sun (point a) is much faster than when it is far away (point b). Note that this means that gravity does work in an elliptical orbit – KE is changing.
Escape Velocity If we want an object to escape an orbit, we need to make sure that it has total energy greater than 0. We can plug this in and find the velocity at a given distance r which is necessary to escape; this is the escape velocity v (^) e.
E = K + U > 0
1 2 mve
(^2) GMm r
1 2 mve
(^2) > GMm r
ve >
r
Rotational Kinematics – Recall that when we use angular variables, they usually must be with radians in order for the formulas to be simple. The figure shows a piece of circular motion.
Recall that if we use radians to describe the angle , then we can write s = R. If we now look at how fast the angle changes, that is, we
take the time derivative of this equation we get ds dt
= v (^) t = d dt
R = R.
The angular velocity is very useful in rotational motion, because while all the individual pieces of an object are moving with different regular velocities, they all have the same angular velocity. For example, a vinyl LP on a turntable has one angular velocity (33. rpm) but the outer edge is moving much faster around than the inner edge.
Finally if we let the angular velocity change, we get an angular acceleration usually denoted with the greek letter . It is defined analogously to regular acceleration, as the time derivative of the
angular velocity: a (^) t = dv^ t dt
= d^ dt
R = R.
Since the angular position, velocity, and acceleration are related by regular time derivatives, we can immediately write down the formulas for constant acceleration using the analogy with the regular constant acceleration formulas:
2
2
2
Before turning to rotational dynamics, we’ll next discuss the point about which objects rotate.