Formulation of orbital kinetic energy

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Woodles
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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.
 
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