Central Force Problem: Nature of Orbits for F=-ar/(r^3) & U=-(a/r)

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SUMMARY

The discussion focuses on the nature of orbits under the central force defined by F=-ar/(r^3) and the corresponding potential energy U=-(a/r). For the case where a>0, the analysis concludes that the orbit is elliptical, as the total energy E is negative. Conversely, when a<0, the force becomes attractive, leading to a hyperbolic trajectory due to the positive total energy. The derivation utilizes the relationships between kinetic energy K, potential energy U, and total energy E to establish these conclusions.

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Homework Statement



Central force F=-ar/(r^3) & Central potential energy,U=-(a/r)
(not U_eff)
Find the nature of orbits if (i)a>0 and (ii)a<0

Homework Equations


The Attempt at a Solution



If we remember the attractive central force E=E(r) diagram,i.e.the one showing the graph of U_eff,we only need to know E_total=K+U.
Where only PE is given.
We see,

U= -integration[F.dr]=integration[dW]=-integration[dK]=-K

Then K=a/r and U=-(a/r)

So,the E=K+U=0

Then in positive and negative both caes we get a parabolic orbit.

Please check if i am correct.
 
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Consider a>0.
Then, -(m(v^2)/r)=-(a/r^2)
or,m(v^2)=(a/r)
Hence total energy E=K+U= -(1/2)(a/r)

=>elliptic orbit.

Consider a<0.

Then,F=+b/r where b=-a>0
and U_p=b/r

K is itrinsically positive.So,total energy positive.

From e=sqrt[1+{(2L^2*E)/(m*b^2)}]
e>1.
hence hyperbolic trajectory.
 

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