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

AI Thread Summary
The discussion explores the nature of orbits under a central force defined by F=-ar/(r^3) and potential energy U=-(a/r). For a>0, the analysis indicates that the total energy is negative, resulting in an elliptical orbit. Conversely, for a<0, the force becomes attractive, leading to a positive total energy and a hyperbolic trajectory. The calculations confirm that both cases yield distinct orbital shapes based on the sign of 'a'. The conclusions emphasize the relationship between force, potential energy, and the resulting orbital characteristics.
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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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