Formulation of orbital kinetic energy

Join the discussion
Registration is free. Start your own thread to ask a follow-up.
1 reply · 2K views
Woodles
Messages
3
Reaction score
0
For a radial potential proportional to r^k, the virial theorem says [itex]\bar{T}=c(k)\bar{V}[/itex]. My problem says to show that c(k)=k/2 for a circular orbit.

I actually solved the problem all ready (by setting the gradiant of the potential equal to the centripetal force and solving for 1/2*m*v^2.)

However, while I was looking around, I came across something.

I found a formulation of kinetic energy saying that [itex]\bar{T}= 1/2 \vec{∇}(V) .\vec{r}[/itex].

How could you derive this? Is it true? Why? The original post said this came from the virial theorem.
 
Physics news on Phys.org
Just integrate with respect to time in the LHS and you'll get it.

[tex]\frac{m}{2} \int_{t_1}^{t_2} \frac{dr}{dt}\left(\frac{dr}{dt} dt\right) = ...[/tex]